US20190162350A1 - Inline fluid damper device - Google Patents
Inline fluid damper device Download PDFInfo
- Publication number
- US20190162350A1 US20190162350A1 US15/827,587 US201715827587A US2019162350A1 US 20190162350 A1 US20190162350 A1 US 20190162350A1 US 201715827587 A US201715827587 A US 201715827587A US 2019162350 A1 US2019162350 A1 US 2019162350A1
- Authority
- US
- United States
- Prior art keywords
- flow
- conduit
- fluid
- damper device
- center axis
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000012530 fluid Substances 0.000 title claims abstract description 241
- 239000000446 fuel Substances 0.000 description 14
- 239000000463 material Substances 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 230000009467 reduction Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 1
- 230000001427 coherent effect Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007717 exclusion Effects 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L55/00—Devices or appurtenances for use in, or in connection with, pipes or pipe systems
- F16L55/04—Devices damping pulsations or vibrations in fluids
- F16L55/041—Devices damping pulsations or vibrations in fluids specially adapted for preventing vibrations
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/0011—Constructional details; Manufacturing or assembly of elements of fuel systems; Materials therefor
- F02M37/0041—Means for damping pressure pulsations
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L11/00—Hoses, i.e. flexible pipes
- F16L11/26—Hoses, i.e. flexible pipes made of sound-absorbing materials or with sound-absorbing structure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L55/00—Devices or appurtenances for use in, or in connection with, pipes or pipe systems
- F16L55/04—Devices damping pulsations or vibrations in fluids
- F16L55/045—Devices damping pulsations or vibrations in fluids specially adapted to prevent or minimise the effects of water hammer
- F16L55/05—Buffers therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M2200/00—Details of fuel-injection apparatus, not otherwise provided for
- F02M2200/31—Fuel-injection apparatus having hydraulic pressure fluctuations damping elements
- F02M2200/315—Fuel-injection apparatus having hydraulic pressure fluctuations damping elements for damping fuel pressure fluctuations
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/02—Influencing flow of fluids in pipes or conduits
Definitions
- the subject matter described herein relates to devices for attenuating fluid fluctuations.
- An assembly such as a gas turbine engine assembly and associated components are subjected to mechanical vibrations when the engine is operating. Mechanical vibrations in the engine assembly may cause the fuel lines, along with the fluid that passes through the fuel lines, to vibrate.
- mechanical vibrations of an engine assembly cause the fluid in the fuel lines to fluctuate. Pressure fluctuations or flow fluctuations in the fluid may manifest as combustion instabilities of the engine assembly. Additionally, pressure and flow fluctuations in the fluid can create a feedback loop of instability creating further mechanical vibrations in the fluid, fuel lines, or the engine assembly. The mechanical vibrations caused by the feedback loop of instability together with the mechanical vibrations caused by the operating engine may create coherent acoustic coupling fluctuations in the fluid.
- an inline fluid damper device in one embodiment, includes a flow-through conduit configured to be placed inside a larger exterior conduit through which a fluid flows.
- the flow-through conduit is elongated and extends around a center axis.
- the damper device also includes an indirect flow conduit coupled with the flow-through conduit.
- the indirect flow conduit is also configured to be placed inside the larger exterior conduit.
- the flow-through conduit and the indirect flow conduit are configured to dampen one or more flow fluctuations or pressure fluctuations in the fluid flowing in the larger exterior conduit by dividing the fluid into a first portion that flows along the center axis through the flow-through conduit and a second portion that concurrently flows outside of the flow-through conduit along the center axis and along a different direction.
- an inline fluid damper device includes plural elongated stems that couple with each other at plural nodes.
- the stems form an elongated flow-through conduit extending around a center axis.
- the flow-through conduit is configured to be placed inside a larger exterior conduit through which a fluid flows.
- the stems are configured to dampen one or more of flow fluctuations or pressure fluctuations in the fluid flowing in the larger exterior conduit by dividing the fluid such that at least some of the fluid flows through the flow-through conduit without contacting the stems and at least some of the fluid concurrently flows through the flow-through conduit and contacts the stems.
- an inline fluid damper device in one embodiment, includes a flow-through conduit configured to be placed inside a larger exterior conduit through which a fluid flows.
- the flow-through conduit is elongated and extends around a center axis.
- the damper device also includes an indirect flow conduit coupled with the flow-through conduit.
- the indirect flow conduit is also configured to be placed inside the larger exterior conduit.
- the flow-through conduit and the indirect flow conduit are configured to dampen one or more flow fluctuations or pressure fluctuations in the fluid flowing in the larger exterior conduit by dividing the fluid into a first portion that flows along the center axis through the flow-through conduit and a second portion that concurrently flows outside of the flow-through conduit along the center axis and along a different direction.
- the flow-through conduit is configured to extend from a first end to a second end.
- the indirect flow conduit creates a longer flow path for the second portion of the fluid to flow from the first end to the second end relative to a flow path created by the flow-through conduit for the first portion of the fluid to flow from the first end to the second end.
- FIG. 1 illustrates an assembly in accordance with one embodiment
- FIG. 2 illustrates a perspective view of an inline fluid damper device in accordance with one embodiment
- FIG. 3 illustrates a cross-sectional view of the inline fluid damper device of FIG. 2 in accordance with one embodiment
- FIG. 4 illustrates a perspective view of an inline fluid damper device in accordance with one embodiment
- FIG. 5 illustrates a perspective view of an inline fluid damper device in accordance with one embodiment
- FIG. 6 illustrates a perspective view of an inline fluid damper device in accordance with one embodiment
- FIG. 7 illustrates a cross-sectional perspective view of an inline fluid damper device in accordance with one embodiment
- FIG. 8 illustrates a cross-sectional perspective view of an inline fluid damper device in accordance with one embodiment
- FIG. 9 illustrates a translucent perspective view of an inline fluid damper device in accordance with one embodiment
- FIG. 10A illustrates a perspective view of an inline fluid damper device in accordance with one embodiment
- FIG. 10B illustrates a front view of the inline fluid damper device of FIG. 10A in accordance with one embodiment
- FIG. 11A illustrates a perspective view of an inline fluid damper device in accordance with one embodiment
- FIG. 11B illustrates a front view of the inline fluid damper device of FIG. 11A in accordance with one embodiment
- FIG. 12 illustrates a flowchart of a method in accordance with one embodiment.
- One or more embodiments of the subject matter described herein relate to devices that dampen flow fluctuations or pressure fluctuations in a fluid that is flowing through a larger exterior conduit.
- the devices include an inline fluid damper device that is placed inside of the larger exterior conduit.
- the damper device includes one or more interior conduits that divide the fluid that is flowing through the exterior conduit into one or more portions. The divided fluid flows along a center axis and in one or more different directions along one or more flow paths created by the interior conduits.
- One technical effect of the subject matter described herein is improved reduction of fluid pressure or flow fluctuations responsive to mechanical vibrations caused by the engine assembly in operation.
- the systems and methods described herein may improve the reduction of fuel line pressure fluctuations or fuel line flow fluctuations in the fluid responsive to the fluid being unsteady or responsive to the engine assembly creating and/or causing mechanical vibrations, or the like.
- FIG. 1 illustrates an assembly 10 in accordance with one embodiment.
- the system 10 includes an exterior conduit 54 that is coupled between a system 12 and a reservoir 52 .
- the exterior conduit 54 is a conduit (e.g., channel, tube, hose, pipe, or the like) that delivers fluid from the reservoir 52 to the system 12 .
- the exterior conduit 54 may be a fuel line and the system 12 may be an engine system.
- the exterior conduit 54 may provide the passage of fuel from the reservoir 52 to a combustor of the engine system.
- the system 12 may be any alternative mechanical system and the exterior conduit 54 may pass any fluid between the reservoir 52 and the system 12 .
- the exterior conduit 54 may be rigid, flexible, or a combination of rigid and flexible along the length of the exterior conduit 54 between the reservoir 52 and the system 12 .
- plural exterior conduits 54 may be operably coupled with the reservoir 52 , the system 12 , an alternative reservoir (not shown), a second system, another component, or any combination therein.
- An inline fluid damper device 100 is disposed inside the exterior conduit 54 at a location between the reservoir 52 and the system 10 .
- the inline fluid damper device 100 is located upstream of the system 10 .
- the exterior conduit 54 may be referred to as a larger exterior conduit 54 such that the larger exterior conduit 54 has a cross-sectional area that is larger relative to the size and/or shape of the damper device 100 .
- the damper device 100 is sized and shaped in order to be entirely contained within the larger exterior conduit 54 .
- the damper device 100 is disposed at a position that is closer to the reservoir 52 than the system 12 .
- the damper device 100 may be disposed at any location between the reservoir 52 and the system 12 .
- one or more damper devices 100 may be disposed inside of the larger exterior conduit 54 .
- a first damper device 100 may be disposed closer to the reservoir 52 and a second damper device may be disposed closer to the system 12 such that the fluid sequentially flows through the first damper device then the second damper device between the reservoir 52 and the system 12 .
- one or more damper devices 100 may be disposed inside of the fuel line 54 at any location, in any configuration, or the like.
- the damper device 100 is configured to substantially fill an interior chamber of the larger exterior conduit 54 .
- the damper device 100 may not substantially fill the interior chamber of the larger exterior conduit 54 .
- FIG. 2 illustrates a perspective view of the inline fluid damper device 100 in accordance with one embodiment.
- the damper device 100 includes one or more interior conduits that are placed inside of the larger exterior conduit 54 .
- the inline fluid damper device 100 includes two interior conduits 204 , 210 .
- the interior conduit 204 may be referred to herein as a flow-through conduit 204
- the interior conduit 210 may be referred to as an indirect flow conduit 210 .
- the damper device 100 may include plural flow-through conduits 204 and/or plural indirect flow conduits 210 .
- the flow-through conduit 204 extends a length L between a first end 206 and a second end 208 .
- the flow-through conduit 204 is a channel or passage through which fluid flows between the first end 206 and the second end 208 .
- the damper device 100 may include two or more flow-through conduits 204 through which fluid flows between the first and second ends 206 , 208 .
- the flow-through conduit 204 is elongated along and extends around a center axis 202 . In the illustrated embodiment, the flow-through conduit 204 is substantially centered about the center axis 202 between the first and second ends 206 , 208 .
- the flow-through conduit 204 may not be centered about the center axis 202 along the length L. Additionally or alternatively, the flow-through conduit 204 may extend along a different axis.
- the flow-through conduit 204 may be substantially centered about the center axis 202 at a position near the first end 206 , and may not be substantially centered about the center axis 202 at a position near the second end 208 . Additionally or alternatively, the flow-through conduit 204 may extend along a different axis that is substantially parallel with the center axis 202 .
- the flow-through conduit 204 has a substantially circular cross-sectional shape and is tubular between the first and second ends 206 , 208 .
- the flow-through conduit 204 may have any alternative cross-sectional shape such as, but not limited to, quadrilateral, oval, or the like.
- the flow-through conduit 204 may have one or more different and/or varying cross-sectional shapes along the length L between the first end 206 and the second end 206 .
- the conduit 204 may have a circular cross-sectional shape at a position near the first end 206 and may have a quadrilateral cross-sectional shape at a position near the second end 208 , may have a circular cross-sectional shape near the first end 206 and a concentric smaller or larger circular cross-sectional shape near the second end 208 , or the like.
- the indirect flow conduit 210 is operably coupled with the flow-through conduit 204 and disposed outside of the flow-through conduit 204 .
- the indirect flow conduit 210 extends a length SL along the center axis 202 .
- the length SL is less than the length L of the flow-through conduit 204 .
- the length SL may be substantially equal to the length L.
- the indirect flow conduit 210 may begin substantially at or near the first end 206 , may end substantially at or near the second end 208 , or a combination therein.
- the indirect flow conduit 210 includes a spiral protrusion 216 that is helically wrapped around the flow-through conduit 204 .
- the spiral protrusion 216 radially protrudes from the flow-through conduit 204 away from the center axis 202 .
- the spiral protrusion 216 protrudes away from the flow-through conduit 204 in a radial direction generally perpendicular to or otherwise away from the center axis 202 .
- one or more of the spirals of the spiral protrusion may extend in any direction away from the flow-through conduit 204 .
- the spiral protrusion 216 is helically wrapped seventeen times around the flow-through conduit 204 and each protrusion is disposed equidistance apart from each other along the length SL.
- the spiral protrusion 216 may include any number of helically wrapped spirals. Additionally or alternatively, any number of the spiral protrusions may be positioned equidistance or non-equidistance apart from each other along the length SL. Additionally, each spiral extends substantially equal distances radially away from the flow-through conduit 204 . Optionally, one or more of the spirals may extend a distance less than or greater than one or more alternative spirals.
- the spiral protrusion 216 extends the length SL that is less than the length L of the flow-through conduit 204 .
- the spiral protrusion 216 is helically wrapped around the flow-through conduit 204 at least partially between the first end 206 and the second end 208 of the flow-through conduit 204 along the center axis 202 .
- the spiral protrusion 216 may be helically wrapped around the flow-through conduit 204 a length that is substantially equal to the length L between the first and second ends 206 , 208 .
- the spiral protrusion 216 extends a continuous length along the length SL of the indirect flow conduit 210 .
- one or more spiral protrusions 216 may extend one or more common and/or unique non-continuous lengths.
- one or more spiral protrusions 216 may have any alternative configuration.
- the damper device 100 is a unitary device that includes the flow-through conduit 204 integrally formed with the indirect flow conduit 210 as a single device manufactured of a common material.
- the damper device 100 including the flow-through conduit 204 and the indirect flow conduit 210 , may be die-cast, injection molded, machined, or the like.
- one or more of the interior conduits e.g., the flow-through conduit 204 or the indirect flow conduit 210
- the indirect flow conduit 210 may be welded to, printed on, mechanically fastened to, or the like, the flow-through conduit 204 .
- the flow-through conduit 204 may be manufactured out of a material that is unique to the material of the indirect flow conduit 210 .
- the damper device may be manufactured by any alternative methods.
- the damper device 100 and/or one or more of the flow-through conduit 204 or the indirect flow conduit 210 may be manufactured of a metallic alloy or a non-metallic material.
- the damper device 100 may be a flexible or rigid device.
- the damper device 100 may be flexible such that the device 100 may flex in order to conform to the larger exterior conduit 54 .
- FIG. 3 illustrates a cross-sectional view of the inline fluid damper device 100 that is disposed inside of the larger exterior conduit 54 in accordance with one embodiment.
- the spiral protrusion 216 radially protrudes distances 310 , 312 between the flow-through conduit 204 .
- the spiral protrusion 216 is operably coupled with the flow-through conduit 204 at an outer surface 304 of the flow-through conduit 204 .
- the spiral protrusion 216 extends distances 310 , 312 from the outer surface 304 of the flow-through conduit 204 to an inner surface 306 of the larger exterior conduit 54 .
- FIG. 3 illustrates a cross-sectional view of the inline fluid damper device 100 that is disposed inside of the larger exterior conduit 54 in accordance with one embodiment.
- the spiral protrusion 216 radially protrudes distances 310 , 312 between the flow-through conduit 204 .
- the spiral protrusion 216 is operably coupled with the flow-through conduit 204 at an outer
- the flow-through conduit 204 is generally centered about the center axis 202 , and the spiral protrusion 216 radially protrudes away from the flow-through conduit 204 .
- the distance 310 may be greater than (e.g., a larger distance) or less than (e.g., a shorter distance) than the distance 312 between the outer surface 304 and the inner surface 306 .
- the flow-through conduit 204 and the spiral protrusion 216 may not be generally centered about the center axis 202 .
- the damper device 100 placed inside of the larger exterior conduit 54 divides the fluid that is flowing in a direction A from the reservoir 52 into a first portion 212 and a second portion 214 .
- the first portion 212 of the fluid flows along the center axis 202 through the flow-through conduit 204 from the first end 206 to the second end 208 .
- the first portion 212 may flow in a direction from the second end 208 to the first end 206 .
- the second portion 214 of the fluid flows outside of the flow-through conduit 204 along the center axis 202 and along a different direction.
- the second portion 214 of the fluid flows in a direction around the spiral protrusion 216 of the indirect flow conduit 210 along the center axis 202 .
- the first and second portions 212 , 214 of the fluid may contain substantially the same or substantially different volumes of the fluid.
- the flow-through conduit 204 may be sized and shaped such that the flow-through conduit 204 may allow more or less fluid (e.g., a larger or smaller volume of fluid) to be divided into the first portion 212 relative to the second portion 214 .
- the first portion 212 of the fluid flows through the flow-through conduit 204 concurrently with the second portion 214 of the fluid that flows outside of the flow-through conduit 204 (e.g., along the path created by the indirect flow conduit 210 ), respectively.
- the fluid flowing in the direction A that is divided into the first and second portions 212 , 214 flows through the flow-through conduit 204 and outside of the flow-through conduit 204 (e.g., along the flow path of the indirect flow conduit 210 ) at substantially the same time.
- the indirect flow conduit 210 creates a longer flow path for the second portion 214 of the fluid to flow from the first end 206 to the second end 208 relative to the flow path created by the flow-through conduit 204 for the first portion 212 of the fluid to flow from the first end 206 to the second end 208 .
- the time it takes for the second portion 214 of the fluid to flow along the path created by the indirect flow conduit 210 is longer (e.g., a larger or greater amount of time) relative to the time it takes for the first portion 212 of the fluid to concurrently flow (e.g., flow at substantially the same time) along the path created by the flow-through conduit 204 .
- FIG. 4 illustrates a perspective view of an inline fluid damper device 400 in accordance with one embodiment.
- the damper device 400 includes a rod 420 and an interior conduit 410 .
- the interior conduit 410 may be referred to herein as an indirect flow conduit 410 .
- the rod 420 extends a length L between a first end 406 and a second end 408 along the center axis 202 .
- the indirect flow conduit 410 extends a length SL along the center axis 202 . In the illustrated embodiment, the length SL is less than the length L of the rod 420 . Additionally or alternatively, the length SL may be substantially equal to the length L.
- the indirect flow conduit 410 may begin substantially at the first end 406 , may end substantially at the second end 408 , or a combination therein.
- the indirect flow conduit 410 includes a spiral protrusion 416 that is helically wrapped around the rod 420 .
- the spiral protrusion 416 is helically wrapped seventeen times around the rod 420 and each protrusion is disposed equidistance apart from each other protrusion along the length SL.
- the spiral protrusion 416 may include any number of helically wrapped spirals that are spaced any uniform and/or non-uniform distances apart from each other.
- each spiral of the spiral protrusion 416 radially protrudes a common distance away from an exterior surface 424 of the rod 420 .
- each spiral of the spiral protrusion 416 extends radially away from the center axis 202 between the exterior surface 424 and an inner surface of the larger exterior conduit 54 (e.g., inner surface 306 ).
- one or more spirals may not extend to the inner surface of the exterior conduit 54 .
- the damper device 400 is placed inside of the larger exterior conduit 54 and directs the fluid that is flowing in a direction A from the reservoir into a portion 414 .
- the portion 414 of the fluid flows outside of the rod 420 along the center axis 202 and in a direction around the spiral protrusion 416 of the indirect flow conduit 410 along the center axis 202 .
- the spiral protrusion 416 of the indirect flow conduit 410 creates a longer flow path for the portion 414 of the fluid to flow from the first end 406 to the second end 408 relative to a flow path that is devoid the spiral protrusion 416 .
- the indirect flow conduit 410 of the damper device 400 creates a flow path for the fluid to flow such that the fluid flowing in the direction A flows slower along the flow path created by the indirect flow conduit 410 relative to the flow of the fluid outside of the indirect flow conduit 410 and inside of the larger exterior conduit 54 (e.g., before and/or after the fluid flows through the indirect flow conduit 410 ).
- the spiral protrusion 416 of the indirect flow conduit 410 may be shaped and/or sized in order to change the speed of the fluid that flows through the damper device 400 .
- FIG. 5 illustrates a perspective view of an inline fluid damper device 500 in accordance with one embodiment.
- the damper device 500 includes interior conduits 504 , 510 A, 510 B.
- the interior conduit 504 may be referred to herein as a flow-through conduit 504
- the conduit 510 A may be referred to herein as a first indirect flow conduit 510 A
- the conduit 510 B may be referred to herein as a second indirect flow conduit 510 B.
- the flow-through conduit 504 extends a length L between a first end 506 and a second end 508 along the center axis 202 .
- the first and second indirect flow conduits 510 A, 510 B are operably coupled with the flow-through conduit 504 and are disposed outside of the flow-through conduit 504 .
- the first indirect flow conduit 510 A extends a length SL-A along the center axis 202 and the second indirect flow conduit 510 B extends a length SL-B along the center axis 202 .
- the length SL-A is substantially equal to the length SL-B.
- the first indirect flow conduit 510 A may extend a length SL-A that may be less than or greater than the length SL-B of the second indirect flow conduit 510 B.
- the lengths SL-A, SL-B are separated by a distance 522 in a direction along the center axis 202 .
- the lengths SL-A, SL-B may be separated by a distance greater than or less than the distance 522 .
- the first and second indirect flow conduits 510 A, 510 B include spiral protrusions 516 A, 516 B, respectively, that are helically wrapped around the flow-through conduit 504 .
- the spiral protrusions 516 A, 516 B radially protrude from an outer surface 524 of the flow-through conduit 504 away from the center axis 202 .
- the spiral protrusion 516 A of the first indirect flow conduit 510 A is helically wrapped five times around the flow-through conduit 504
- the spiral protrusion 516 B of the second indirect flow conduit 510 B is helically wrapped five times around the flow-through conduit 504 .
- the first and/or second indirect flow conduits 510 A, 510 B may include less than five or more than five spirals wrapped around the flow-through conduit 504 .
- the damper device 500 placed inside of the larger exterior conduit 54 divides the fluid that is flowing in the direction A into a first portion 512 and a second portion 514 .
- the first portion 512 flows along the center axis 202 through the flow-through conduit 504 between the first end 506 and the second end 508 .
- the second portion 514 flows outside of the flow-through conduit 504 along the center axis 202 and along a different direction.
- the second portion 514 flows in a direction around the spiral protrusions 516 of the first and second indirect flow conduits 510 A, 510 B.
- the second portion 514 of the fluid flows along the flow path created by the spiral protrusion 516 A of the first indirect flow conduit 510 A and then along the flow path created by the spiral protrusion 516 B of the second indirect flow conduit 510 B.
- the flow paths created by the spiral protrusions 516 of the first and second indirect flow conduits 510 A, 510 B rotatably extend in a common direction around the center axis 202 (e.g., in a clockwise direction).
- the spiral protrusions of the first and/or second indirect flow conduits 510 A, 510 B may create a flow path that flows in a unique direction around the center axis 202 .
- the second portion 514 A of the fluid may first flow in a clockwise direction around the spiral protrusion 516 A of the first indirect flow conduit 510 A and then the second portion 514 B may flow in a counter-clockwise direction around the spiral protrusion 516 B of the second indirect flow conduit 510 B, or any alternative combination therein.
- the damper device 500 may include more than two indirect flow conduits 510 that may direct the second portion 514 of the fluid to flow in any direction.
- the first portion 512 of the fluid flows through the flow-through conduit 504 concurrently with the second portion 514 of the fluid that flows outside of the flow-through conduit 504 (e.g., along the path created by the first and second indirect flow conduits 510 A, 510 B).
- the fluid flowing in the direction A that is divided into the first and second portions 512 , 514 flows along the flow paths created by the flow-through conduit 504 and the first and second indirect flow conduits 510 A, 510 B at substantially the same time.
- first and second indirect flow conduits 510 A, 510 B create a longer flow path for the second portion 514 of the fluid to flow from the first end 506 to the second end 508 relative to the flow path created by the flow-through conduit 504 for the first portion 512 of the fluid to flow from the first end 506 to the second end 508 .
- the time it takes for the second portion 514 of the fluid to flow along the flow path created by the indirect flow conduits 510 A, 510 B is longer (e.g., a larger or greater amount of time) relative to the time it takes for the first portion 512 of the fluid to concurrently flow along the flow path created by the flow-through conduit 504 .
- FIG. 6 illustrates a perspective view of an inline fluid damper device 600 in accordance with one embodiment.
- the damper device 600 includes interior conduits 604 and 610 .
- the interior conduit 604 may be referred to herein as a flow-through conduit 604
- the interior conduit 610 may be referred to herein as an indirect flow conduit 610 .
- the flow-through conduit 604 is elongated along and generally centered about the center axis 202 between first and second ends 606 , 608 .
- the damper device 600 may include two or more flow-through conduits 604 that may be operably coupled with each other flow-through conduit 604 and may be elongated along the center axis 202 , or any combination therein.
- the indirect flow conduit 610 is operably coupled with the flow-through conduit 604 and disposed outside of the flow-through conduit 604 .
- two or more indirect flow conduits 610 may be operably coupled with and disposed outside of the flow-through conduit 604 .
- the indirect flow conduit 610 includes a spiral protrusion 616 that is helically wrapped around the flow-through conduit 604 .
- the spiral protrusion 616 radially protrudes from an outer surface 624 of the flow-through conduit 604 away from the center axis 202 .
- the spiral protrusion 616 includes plural baffles 622 that are disposed along the length SL of the indirect flow conduit 610 .
- the baffles 622 extend between and operably couple two or more of the spirals of the spiral protrusion 616 along the length SL.
- the baffles 622 may be referred to as steps or plates that protrude in a direction generally parallel to the elongated direction of the damper device 600 .
- the baffles 622 may protrude in any direction between two or more spirals.
- the damper device 600 placed inside of the larger exterior conduit 54 divides the fluid that is flowing in the direction A into a first portion 612 and a second portion 614 .
- the first portion flows along the center axis 202 through the flow-through conduit 604 .
- the second portion 614 flows outside of the flow-through conduit 604 and along a flow path that is created by the baffles 622 and spirals of the spiral protrusion 616 of the indirect flow conduit 610 .
- the indirect flow conduit 610 creates a longer flow path for the second portion 614 of the fluid to flow from the first end 606 to the second end 608 relative to the flow path created by the flow-through conduit 604 for the first portion 612 of the fluid to flow from the first end 606 to the second end 608 .
- the time is takes for the second portion 614 of the fluid to flow along the flow path created by the indirect flow conduit 610 is longer (e.g., a larger or greater amount of time) relative to the time it takes for the first portion 612 of the fluid to concurrently flow along the flow path created by the flow-through conduit 604 .
- FIG. 7 illustrates a cross-sectional perspective view of an inline fluid damper device 700 in accordance with one embodiment.
- the damper device 700 includes interior conduits 704 and 710 .
- the interior conduit 704 may be referred to herein as a flow-through conduit 704
- the interior conduit 710 may be referred to herein as an indirect flow conduit 710 .
- the flow-through conduit 704 is elongated along and generally centered about the center axis 202 between first and second ends 706 , 708 .
- the flow-through conduit 704 includes an inner surface 726 and an outer surface 724 .
- the flow-through conduit 704 includes a rod 720 that is elongated along and is generally centered about the center axis 202 .
- the rod 720 is a solid or closed rod.
- the rod 720 may be an open passage or channel between the first end 706 and the second end 708 .
- the flow-through conduit 704 also includes an inner spiral protrusion 728 that is operably coupled with the inner surface 726 of the flow-through conduit 704 .
- the inner spiral protrusion 728 is helically wrapped around the rod 720 between the first and second ends 706 , 708 .
- the inner spiral protrusion 728 includes five spirals that are disposed substantially equidistance apart from each other.
- the inner spiral protrusion 728 may include any number of spirals, the spirals may be spaced apart any common or unique distances, the spirals may have a multi-spiral counter-rotating configuration, may have a multi-spiral co-rotating configuration, or any combination therein.
- the indirect flow conduit 710 is operably coupled with the outer surface 724 of the flow-through conduit and is disposed outside of the flow-through conduit 704 .
- two or more indirect flow conduits 710 may be operably coupled with and disposed outside of the flow-through conduit 704 .
- the indirect flow conduit 710 includes a spiral protrusion 716 that is helically wrapped around the flow-through conduit 704 .
- the spiral protrusion 716 radially protrudes from the outer surface 724 of the flow-through conduit 704 away from the center axis 202 .
- the damper device 700 placed inside of the larger exterior conduit 54 divides the fluid into a first portion 712 and a second portion 714 .
- the first portion 712 flows through the flow-through conduit 704 and along the flow path created by the rod 720 and the inner spiral protrusion 728 .
- the first portion 712 of the fluid flows through the flow-through conduit 704 along the center axis 202 in a rotating counter-clockwise direction from the first end 706 to the second end 708 .
- the second portion 714 flows outside of the flow-through conduit 704 and along a flow path that is created by the spirals of the spiral protrusion 716 .
- the second portion 714 of the fluid flows outside of the flow-through conduit 704 along the center axis 202 in a rotating clockwise direction from the first end 706 to the second end 708 .
- the inner spiral protrusion 728 and the spiral protrusion 716 may be helically wrapped around the flow-through conduit 704 such that the first portion 712 of the fluid and the second portion 714 of the fluid flow in the same rotating direction from the first end 706 to the second end 708 .
- the inner spiral protrusion 728 may be shaped in order to create a flow path for the first portion 712 of the fluid to flow in a same rotating direction as the flow path for the second portion 714 that is created by the spiral protrusion 716 .
- the spiral protrusion 716 of the indirect flow conduit 710 is shaped and/or sized in order to create a longer flow path for the second portion 714 of the fluid to flow from the first end 706 to the second end 708 relative to flow path created by the inner spiral protrusion 728 of the flow-through conduit 704 for the first portion 712 of the fluid to concurrently flow from the first end 706 to the second end 708 .
- the inner spiral protrusion 728 and/or the rod 720 of the flow-through conduit 704 may be shaped and/or sized in order to create a longer flow path for the first portion 712 for the fluid to flow relative to the second portion 714 of the fluid.
- the inner spiral protrusion 728 may be shaped and/or sized in order to create a flow path for the first portion 712 that has a length that is substantially the same as a length of the flow path created by the spiral protrusion 716 of the indirect flow conduit 710 .
- the flow-through conduit 704 and the indirect flow conduit 710 may be shaped/sized in order for the first and second portions 712 , 714 of the fluid to concurrently flow through the damper device 700 in substantially the same amount of time or in different amounts of time.
- FIG. 8 is a cross-sectional perspective view of an inline fluid damper device 800 in accordance with one embodiment.
- the damper device 800 includes an interior conduit 804 .
- the interior conduit 804 may be referred to as a flow-through conduit 804 .
- the flow-through conduit 804 is elongated along the center axis 202 between first and second ends 806 , 808 .
- the flow-through conduit 804 includes an inner surface 826 and an outer surface 824 .
- the damper device 800 includes a plate 820 that is disposed inside of the flow-through conduit 804 .
- the plate 820 is elongated along and generally centered about the center axis 202 .
- the plate 820 extends between a first end 842 that is disposed near the first end 806 of the flow-through conduit 804 and a second end 844 that is disposed near the second end 806 of the flow-through conduit 804 .
- the plate 820 extends a distance between the first and second ends 842 , 844 that is shorter than the length of the flow-through conduit 804 .
- the plate 820 may extend a length that is substantially the same length as the flow-through conduit 804 .
- first end 842 includes a first end baffle 852 and the second end 844 includes a second end baffle 854 .
- the first and second end baffles 852 , 855 protrude a distance away from the plate 820 in a direction generally away from the center axis 202 .
- the plate 820 divides the flow-through conduit 804 into a first flow-through conduit 804 A and a second flow-through conduit 804 B that is substantially equal in shape and size with the first flow-through conduit 804 A between the first and second ends 806 , 808 .
- the first and second flow-through conduits 804 A, 804 B may have substantially the same volume inside of the damper device 800 .
- the plate 820 may not be generally centered about the center axis 202 such that the first and second flow-through conduits 804 A, 804 B are not substantially equal in shape or size.
- the damper device 800 may include any number of plates 820 that may divide the flow-through conduit 804 into any number of divided flow-through conduits.
- the plate 820 has a first side 834 and an opposite second side 836 .
- the first side 834 faces the first flow-through conduit 804 A
- the second side 836 faces towards the second flow-through conduit 804 B.
- the damper device 800 includes one or more exterior baffles 822 that are operably coupled with the inner surface 826 of the flow-through conduit 804 .
- the baffles 822 protrude a distance away from the inner surface 826 of the flow-through conduit 804 and in a direction towards the center axis 202 .
- the exterior baffles 822 extend a distance away from the inner surface 826 in a direction generally perpendicular to the center axis 202 .
- one or more of the exterior baffles 822 may extend in any common or unique direction away from the inner surface 826 .
- the first flow-through conduit 804 A includes five exterior baffles 822 A and the second flow-through conduit 804 B includes eight exterior baffles 822 B. Additionally or alternatively, the first or second flow-through conduits 804 A, 804 B may include any number of exterior baffles 822 .
- the plate 820 includes one or more interior baffles 832 that are operably coupled with the plate 820 and protrude a distance away from the plate 820 in a direction generally away from the plate 820 .
- the plate 820 includes four interior baffles 832 A that are operably coupled with the first side 834 of the plate 820 .
- the four interior baffles 832 A extend a common distance away from the first side 834 of the plate 820 and protrude into the first flow-through conduit 804 A.
- the plate 820 includes seven interior baffles 832 B that are operably coupled with the second side 836 of the plate 820 .
- the seven interior baffles 832 B extend a common distance away from the second side 836 of the plate 820 and protrude into the second flow-through conduit 804 B. Additionally or alternatively, any number of baffles 832 may extend away from the first or second sides 834 , 836 of the plate 820 and protrude into the first or second flow-through conduits 804 A, 804 B.
- the interior baffles 832 extend away from the plate 820 in a direction substantially perpendicular to the center axis 202 . Optionally, any number of baffles 832 may extend in any direction away from the plate 820 .
- the damper device 800 placed inside of the larger exterior conduit 54 divides the fluid into a first portion 812 A and a second portion 812 B.
- the first portion 812 A flows through the first flow-through conduit 804 A and along the flow path created by the interior and exterior baffles 832 A, 822 A that protrude into the first flow-through conduit 804 A.
- the second portion 812 B of the fluid flows through the second flow-through conduit 804 B and along the flow path created by the interior and exterior baffles 832 B, 822 B that protrude into the second flow-through conduit 804 B.
- the second flow-through conduit 804 B includes more interior and exterior baffles 832 B, 822 A than the first flow-through conduit 804 A.
- the second flow-through conduit 804 B is shaped and sized in order to create a longer flow path for the second portion 812 B of the fluid to flow from the first end 806 to the second end 808 relative to the flow path created by the first flow-through conduit 804 A.
- first and second flow-through conduits 804 A, 804 B may include a common number of interior and/or exterior baffles 832 , 822 such that the first and second flow-through conduits 804 A, 804 B create a substantially common flow path for the first and second portions 812 A, 812 B of the fluid to flow.
- FIGS. 2 through 8 illustrate six embodiments of inline fluid damper devices.
- an inline damper device may have any alternative shape, size, configuration, or the like, of one or more flow-through conduits, one or more indirect flow conduits, one or more portions of fluid flowing along one or more flow paths, or the like.
- a dampening system is provided that includes any two or more of the damper devices described herein (the same or different embodiments of the devices) disposed back-to-back or otherwise in a serial relationship such that fuel or other fluids sequentially flow through the multiple damper devices between a fluid reservoir and a load (e.g., an engine).
- FIG. 9 is a translucent perspective view of an inline fluid damper device 1000 in accordance with one embodiment.
- the damper device 1000 includes interior conduits 1004 , 1010 A, 1010 B.
- the interior conduit 1004 may be referred to herein as a flow-through conduit 1004
- the interior conduit 1010 A may be referred to herein as a first indirect flow conduit 1010 A
- the interior conduit 1010 B may be referred to herein as a second indirect flow conduit 1010 B.
- the flow-through conduit 1004 is elongated along the center axis 202 between first and second ends 1006 , 1008 .
- the flow-through conduit 1004 includes an inner surface 1026 and an outer surface 1024 .
- the first and second indirect flow conduits 1010 A, 1010 B include one or more closed loops 1022 that radially protrude from the flow-through conduit 1004 in a direction away from the center axis 202 .
- Each of the closed loops 1022 includes a loop baffle 1020 that is disposed inside of each of the closed loops 1022 .
- the loop baffles 1020 separate the closed loops 1022 of the first and second indirect flow conduits 1010 A, 1010 B from the flow-through conduit 1004 .
- the first indirect flow conduit 1010 A includes three closed loops 1022 A that radially protrude from the flow-through conduit 1004 on a first side of the center axis 202
- the second indirect flow conduit 1010 B includes four closed loops 1022 B that radially protrude from the flow-through conduit 1004 on an opposite, second side of the center axis 202
- the damper device 1000 may include any number of indirect flow conduits 1010 that may include any number of closed loops 1022 that may protrude from any side of the center axis 202 .
- the closed loops 1022 A, 1022 B are arranged in an alternating configuration along the length of the damper device 1000 between the first and second ends 1006 , 1008 .
- the first and second indirect flow conduits 1010 A, 1010 B may include any common or unique number of closed loops 1022 .
- the closed loops 1022 of the first and second indirect flow conduits 1010 A, 1010 B may be arranged in any alternating, random, patterned, continuous configuration, or the like, between the first and second ends 1006 , 1008 .
- the first indirect flow conduit 1010 A may include one or more closed loops 1022 A that may protrude from the flow-through conduit 1004 on the first side of the center axis 202
- the second indirect flow conduit 1010 B may not include any closed loops 1022 B that protrude from the flow-through conduit 1004
- the closed loops 1022 and the first and second indirect flow conduits 1010 A, 1010 B may have any alternative configuration.
- the damper device 1000 placed inside of the larger exterior conduit 54 divides the fluid flowing in the direction A into a first portion 1012 , a second portion 1014 A, and a third portion 1014 B.
- the first portion 1012 of the fluid flows through the flow-through conduit 1004 from the first end 1006 to the second end 1008 .
- the second portion 1014 A of the fluid flows through the first indirect flow conduit 1010 A and around the closed loops 1022 A of the first indirect flow conduit 1010 A.
- the third portion 1014 B of the fluid flows through the second indirect flow conduit 1010 B and around the closed loops 1022 B of the second indirect flow conduit 1010 B.
- the loop baffles 1020 A of the first indirect flow conduit 1010 A directs the flow of the second portion 1014 A of the fluid around the loop baffles 1020 A and around the closed loops 1022 A.
- the loop baffles 1020 B of the second indirect flow conduit 1010 B directs the flow of the third portion 1014 B of the fluid around the loops baffles 1020 B and around the closed loops 1022 B.
- the closed loops 1022 A, 1022 B of the first and second indirect flow conduits 1010 A, 1010 B create a longer flow path for the second portion 1014 A and the third portion 1014 B of the fluid to flow from the first end 1006 to the second end 1008 relative to the flow path created by the flow-through conduit 1004 .
- the first portion 1012 of the fluid that flows through the flow path created by the flow-through conduit 1004 flows from the first end 1006 to the second end 1008 more quickly (e.g., in a shorter amount of time) than the second and third portions 1014 A, 1014 B of the fluid that flow through the flow paths created by the first and second indirect flow conduits 1010 A, 1010 B, respectively.
- FIG. 10A illustrates a perspective view of an inline fluid damper device 1200 in accordance with one embodiment.
- FIG. 10B illustrates a front view of the inline fluid damper device 1200 .
- FIGS. 10A and 10B will be discussed together in detail.
- the inline fluid damper device 1200 includes plural elongated stems 1222 that are coupled with each other at plural nodes 1228 .
- the damper device 1200 may be formed as a unitary damper device and/or as a multiple component damper device.
- the damper device 1200 may be cast as a single, unitary, monolithic device including plural stems that are cast or formed together.
- the stems may be welded, adhered, clipped, fastened, or the like, with each other at the nodes 1228 .
- at least part of the damper device 1200 may be formed as a unitary damper device and one or more stems 1222 may be operably coupled with the at least part unitary damper device.
- the stems 1222 are arranged in a repeating lattice pattern.
- the stems 1222 are substantially uniform in shape and size and are arranged such that the stems 1222 form plural cells that are substantially uniformly spaced apart between the stems 1222 .
- the damper device 1200 may include any number of stems 1222 that may be arranged in any random and/or patterned configuration along the length of the damper device 1200 .
- the damper device 1200 may include any number of stems 1222 of any unique and/or uniform shape and/or size that may be arranged in order to form any unique and/or uniform size of cells between the stems 1222 .
- the plural stems 1222 coupled with each other at the plural nodes 1228 forms a flow-through conduit 1204 .
- the flow-through conduit 1204 is elongated along and substantially centered about the center axis 202 .
- the flow-through conduit 1204 extends between a first end 1206 and a second end 1208 .
- the stems 1222 and nodes 1228 are shaped, sized, and arranged such that the flow-through conduit 1204 is generally centered about the center axis 202 .
- the stems 1222 and nodes 1228 may be arranged in any alternative configuration such that the flow-through conduit 1204 may not be substantially centered about the center axis 202 .
- the damper device 1200 placed inside of the larger exterior conduit 54 divides the fluid flowing in the direction A such that at least some of the fluid flows through the flow-through conduit 1204 without contacting any stems 1222 and/or nodes 1228 and at least some of the fluid concurrently flows through the flow-through conduit 1204 and contacts one or more of the stems 1222 and/or nodes 1228 .
- at least some of the fluid flows in a direction 1212 along the center axis 202 and through the flow-through conduit 1204 such that the fluid that flows in the direction 1212 does not contact, touch, interact with, or the like, with any of the stems 1222 and/or nodes 1228 .
- the fluid flows in a direction 1214 such that the fluid that flows in the direction 1214 does contact, touch, interact with, or the like, one or more of the stems 1222 and/or one or more of the nodes 1228 .
- the stems 1222 coupled at the nodes 1228 create a flow path for the fluid that is flowing in the direction 1214 (e.g., the fluid that contacts the stems 1222 and nodes 1228 ) that is longer relative to a flow path created by the stems 1222 and nodes 1228 for the fluid that is flowing in the direction 1212 (e.g., the fluid that does not contact the stems 1222 or nodes 1228 ).
- the one or more stems 1222 and/or the one or more nodes 1228 may create or increase frictional drag as the fluid flows along the flow path in the direction 1214 and contacts the stems 1222 and/or nodes 1228 relative to the at least some of the fluid that flows along the flow path that does not contact the stems 1222 and/or nodes 1228 (e.g., the fluid that flows in the direction 1212 ).
- FIG. 11A illustrates a perspective view of an inline fluid damper device 1300 in accordance with one embodiment.
- FIG. 11B illustrates a front view of the inline fluid damper device 1300 .
- FIGS. 11A and 11B will be discussed together in detail.
- the damper device 1300 includes plural elongated stems 1322 that are coupled with each other at plural nodes 1328 .
- the damper device 1300 may be formed as a unitary damper device and/or as a multiple component damper device.
- the damper device 1300 may be cast as a single, unitary, monolithic device including plural stems that are cast or formed together.
- the stems 1322 may be welded, adhered, clipped, fastened, or the like, with each other at the nodes 1328 .
- at least part of the damper device 1300 may be formed as a unitary damper device and one or more stems 1322 may be operably coupled with the at least part unitary damper device.
- the stems 1322 are arranged in a random configuration.
- the stems 1322 and nodes 1328 are arranged such that the stems 1322 form plural cells that are of random shape, random size, random distances apart, or the like, between the stems 1322 .
- the damper device 1322 may include any number of stems 1322 that are of any uniform or unique shape and/or size that may be arranged in order to form any uniform and/or unique size of cells between the stems 1322 .
- the plural stems 1322 coupled with each other at the plural nodes 1328 forms an indirect flow conduit 1310 .
- the indirect flow conduit 1310 is elongated along and substantially centered about the center axis 202 .
- the indirect flow conduit 1310 extends between a first end 1306 and a second end 1308 along the center axis 202 .
- the stems 1322 and nodes 1328 are arranged such that one or more of the stems 1322 and one or more of the nodes 1328 intersect with the indirect flow conduit 1310 along the center axis 202 .
- one or more of the stems 1322 protrude distances away from the nodes 1328 such that one or more stems 1322 extend in one or more directions that may be substantially parallel to, may be substantially perpendicular to, may be non-parallel with, may be non-perpendicular with, or the like, the center axis 202 .
- one or more stems 1322 or nodes 1328 may intersect with the center axis 202 at one or more locations along the center axis 202 between the first end 1306 and the second end 1308 .
- the damper device 1300 placed inside of the larger exterior conduit 54 divides the fluid flowing in the direction A such that the fluid flows through the indirect flow conduit 1310 and contacts one or more of the stems 1322 and/or nodes 1328 .
- the fluid flows from the first end 1306 to the second end 1308 and contacts, touches, interacts with, or the like, one or more of the stems 1322 and/or one or more of the nodes 1328 .
- the stems 1322 coupled with each other at the nodes 1328 creates plural flow paths for the fluid that is flowing in the direction A such that the fluid may contact, touch, interact with, or the like, one or more stems 1322 and/or one or more nodes 1328 as the fluid flows from the first end 1306 to the second end 1308 .
- FIG. 12 illustrates a flowchart 1500 of a method in accordance with one embodiment.
- an inline fluid damper device is placed inside of a larger exterior conduit through which a fluid is configured to flow.
- the damper device includes one or more interior conduits.
- the interior conduits may be elongated along and may extend around a center axis.
- the damper device may include one or more flow-through conduits, one or more indirect flow conduits, a combination of one or more flow-through conduits and one or more indirect flow conduits, or the like.
- the interior conduits may include one or more spiral protrusions, one or more closed loops, one or more baffles, one or more stems coupled with each other at one or more nodes, or any combination that may include any number of spiral protrusions, closed loops, baffles, stems, or the like.
- the interior conduits may have any alternative shape, size, orientation, or the like, that may divide the fluid that flows through the larger exterior conduit such that the fluid may flow the length of the damper device along any direction of a flow path created by the interior conduits.
- the fluid flows through the inline fluid damper device that is disposed inside of the larger exterior conduit.
- the fluid may be fuel that flows through a fuel line to a gas turbine engine assembly.
- the fluid may be a coolant that flows to a mechanical system, the fluid may be fuel that flows to any alternative mechanical system, the fluid may be any fluid that is removed from any mechanical system, or the like.
- the fluid flows through the larger exterior conduit and through the damper device, for example from a first end to a second end of the damper device. Additionally or alternatively, fluid may flow from the second end to the first end of the damper device.
- fuel may be removed from the gas turbine engine assembly.
- the larger exterior conduit may be any conduit operably coupled with any assembly through which a fluid may flow.
- the one or more interior conduits of the damper device divides the fluid that flows through the damper device into one or more portions.
- the damper device may include a single interior conduit, and the fluid may flow along a flow path created by the interior conduit.
- the damper device may include two or more interior conduits.
- the damper device may include a flow-through conduit (e.g., the flow-through conduit 204 of FIG. 2 ) and two indirect flow conduits (e.g., the indirect flow conduits 510 of FIG. 5 ).
- the fluid may be divided into three portions such that a first portion may flow along a first flow path created by the flow-through conduit, a second portion may flow along a second flow path created by the first indirect flow conduit that is different from the first flow path, and a third portion may flow along a third flow path created by the second indirect flow conduit that is different from the first and second flow paths.
- the fluid may be divided into any number of portions having substantially similar or substantially different volumes of the fluid.
- one or more of the interior conduits may be shaped and/or sized in order to create one or more flow paths having substantially similar flow paths.
- an inline fluid damper device in one embodiment of the subject matter described herein, includes a flow-through conduit configured to be placed inside a larger exterior conduit through which a fluid flows.
- the flow-through conduit is elongated and extends around a center axis.
- the damper device also includes an indirect flow conduit coupled with the flow-through conduit.
- the indirect flow conduit is also configured to be placed inside the larger exterior conduit.
- the flow-through conduit and the indirect flow conduit are configured to dampen one or more flow fluctuations or pressure fluctuations in the fluid flowing in the larger exterior conduit by dividing the fluid into a first portion that flows along the center axis through the flow-through conduit and a second portion that concurrently flows outside of the flow-through conduit along the center axis and along a different direction.
- the flow-through conduit is also configured to extend from a first end to a second end.
- the indirect flow conduit creates a longer flow path for the second portion of the fluid to flow from the first end to the second end relative to a flow path created by the flow-through conduit for the first portion of the fluid to flow from the first end to the second end.
- the indirect flow conduit includes a spiral protrusion helically wrapped around the flow-through conduit and radially protruding from the flow-through conduit away from the center axis.
- the spiral protrusion that radially protrudes from the flow-through conduit is configured to extend from the flow-through conduit to an inner surface of the larger exterior conduit.
- the spiral protrusion is configured to be helically wrapped around the flow-through conduit at least partially between a first end and a second end of the flow-through conduit along the center axis.
- the spiral protrusion is configured to create a flow path for the second portion of the fluid to flow helically along the spiral protrusion between a first end and a second end of the flow-through conduit.
- the indirect flow conduit includes one or more closed loops radially protruding from the flow-through conduit on opposite sides of the center axis.
- the one or more closed loops creates a longer flow path for the second portion of the fluid to flow from the first end to the second end relative to a flow path created by the flow-through conduit for the first portion of the fluid to flow from the first end to the second end.
- the one or more closed loops that radially protrude from the flow-through conduit are configured to create a flow path for the second portion of the fluid to flow around the one or more closed loops between a first end and a second end of the flow-through conduit.
- an inline fluid damper device includes plural elongated stems that couple with each other at plural nodes.
- the stems form an elongated flow-through conduit extending around a center axis.
- the flow-through conduit is configured to be placed inside a larger exterior conduit through which a fluid flows.
- the stems are configured to dampen one or more of flow fluctuations or pressure fluctuations in the fluid flowing in the larger exterior conduit by dividing the fluid such that at least some of the fluid flows through the flow-through conduit without contacting the stems and at least some of the fluid concurrently flows through the flow-through conduit and contacts the stems.
- the stems are configured to extend from the flow-through conduit to an inner surface of the larger exterior conduit.
- the stems are configured to protrude from the plural nodes in a direction towards the center axis.
- the plural stems are configured to form a lattice extending around the center axis between a first end and a second end of the flow-through conduit.
- an inline fluid damper device in one embodiment of the subject matter described herein, includes a flow-through conduit configured to be placed inside a larger exterior conduit through which a fluid flows.
- the flow-through conduit is elongated and extends around a center axis.
- the damper device also includes an indirect flow conduit coupled with the flow-through conduit.
- the indirect flow conduit is also configured to be placed inside the larger exterior conduit.
- the flow-through conduit and the indirect flow conduit are configured to dampen one or more flow fluctuations or pressure fluctuations in the fluid flowing in the larger exterior conduit by dividing the fluid into a first portion that flows along the center axis through the flow-through conduit and a second portion that concurrently flows outside of the flow-through conduit along the center axis and along a different direction.
- the flow-through conduit is configured to extend from a first end to a second end.
- the indirect flow conduit creates a longer flow path for the second portion of the fluid to flow from the first end to the second end relative to a flow path created by the flow-through conduit for the first portion of the fluid to flow from the first end to the second end.
- the indirect flow conduit includes a spiral protrusion helically wrapped around the flow-through conduit and radially protruding from the flow-through conduit away from the center axis.
- the spiral protrusion is configured to be helically wrapped around the flow-through conduit at least partially between a first end and a second end of the flow-through conduit along the center axis.
- the spiral protrusion is configured to create a flow path for the second portion of the fluid to flow helically along the spiral protrusion between a first end and a second end of the flow-through conduit.
- the spiral protrusion that radially protrudes from the flow-through conduit is configured to extend from the flow-through conduit to an inner surface of the larger exterior conduit.
- the indirect flow conduit includes one or more closed loops radially protruding from the flow-through conduit on opposite sides of the center axis.
- the one or more closed loops creates a longer flow path for the second portion of the fluid to flow from the first end to the second end relative to a flow path created by the flow-through conduit for the first portion of the fluid to flow from the first end to the second end.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Pipe Accessories (AREA)
- Infusion, Injection, And Reservoir Apparatuses (AREA)
- Fluid-Damping Devices (AREA)
Abstract
Description
- The subject matter described herein relates to devices for attenuating fluid fluctuations.
- An assembly, such as a gas turbine engine assembly and associated components are subjected to mechanical vibrations when the engine is operating. Mechanical vibrations in the engine assembly may cause the fuel lines, along with the fluid that passes through the fuel lines, to vibrate.
- One issue with mechanical vibrations of an engine assembly is that the mechanical vibrations cause the fluid in the fuel lines to fluctuate. Pressure fluctuations or flow fluctuations in the fluid may manifest as combustion instabilities of the engine assembly. Additionally, pressure and flow fluctuations in the fluid can create a feedback loop of instability creating further mechanical vibrations in the fluid, fuel lines, or the engine assembly. The mechanical vibrations caused by the feedback loop of instability together with the mechanical vibrations caused by the operating engine may create coherent acoustic coupling fluctuations in the fluid.
- In one embodiment, an inline fluid damper device includes a flow-through conduit configured to be placed inside a larger exterior conduit through which a fluid flows. The flow-through conduit is elongated and extends around a center axis. The damper device also includes an indirect flow conduit coupled with the flow-through conduit. The indirect flow conduit is also configured to be placed inside the larger exterior conduit. The flow-through conduit and the indirect flow conduit are configured to dampen one or more flow fluctuations or pressure fluctuations in the fluid flowing in the larger exterior conduit by dividing the fluid into a first portion that flows along the center axis through the flow-through conduit and a second portion that concurrently flows outside of the flow-through conduit along the center axis and along a different direction.
- In one embodiment, an inline fluid damper device includes plural elongated stems that couple with each other at plural nodes. The stems form an elongated flow-through conduit extending around a center axis. The flow-through conduit is configured to be placed inside a larger exterior conduit through which a fluid flows. The stems are configured to dampen one or more of flow fluctuations or pressure fluctuations in the fluid flowing in the larger exterior conduit by dividing the fluid such that at least some of the fluid flows through the flow-through conduit without contacting the stems and at least some of the fluid concurrently flows through the flow-through conduit and contacts the stems.
- In one embodiment, an inline fluid damper device includes a flow-through conduit configured to be placed inside a larger exterior conduit through which a fluid flows. The flow-through conduit is elongated and extends around a center axis. The damper device also includes an indirect flow conduit coupled with the flow-through conduit. The indirect flow conduit is also configured to be placed inside the larger exterior conduit. The flow-through conduit and the indirect flow conduit are configured to dampen one or more flow fluctuations or pressure fluctuations in the fluid flowing in the larger exterior conduit by dividing the fluid into a first portion that flows along the center axis through the flow-through conduit and a second portion that concurrently flows outside of the flow-through conduit along the center axis and along a different direction. The flow-through conduit is configured to extend from a first end to a second end. The indirect flow conduit creates a longer flow path for the second portion of the fluid to flow from the first end to the second end relative to a flow path created by the flow-through conduit for the first portion of the fluid to flow from the first end to the second end.
- The present inventive subject matter will be better understood from reading the following description of non-limiting embodiments, with reference to the attached drawings, wherein below:
-
FIG. 1 illustrates an assembly in accordance with one embodiment; -
FIG. 2 illustrates a perspective view of an inline fluid damper device in accordance with one embodiment; -
FIG. 3 illustrates a cross-sectional view of the inline fluid damper device ofFIG. 2 in accordance with one embodiment; -
FIG. 4 illustrates a perspective view of an inline fluid damper device in accordance with one embodiment; -
FIG. 5 illustrates a perspective view of an inline fluid damper device in accordance with one embodiment; -
FIG. 6 illustrates a perspective view of an inline fluid damper device in accordance with one embodiment; -
FIG. 7 illustrates a cross-sectional perspective view of an inline fluid damper device in accordance with one embodiment; -
FIG. 8 illustrates a cross-sectional perspective view of an inline fluid damper device in accordance with one embodiment; -
FIG. 9 illustrates a translucent perspective view of an inline fluid damper device in accordance with one embodiment; -
FIG. 10A illustrates a perspective view of an inline fluid damper device in accordance with one embodiment; -
FIG. 10B illustrates a front view of the inline fluid damper device ofFIG. 10A in accordance with one embodiment; -
FIG. 11A illustrates a perspective view of an inline fluid damper device in accordance with one embodiment; -
FIG. 11B illustrates a front view of the inline fluid damper device ofFIG. 11A in accordance with one embodiment; and -
FIG. 12 illustrates a flowchart of a method in accordance with one embodiment. - One or more embodiments of the subject matter described herein relate to devices that dampen flow fluctuations or pressure fluctuations in a fluid that is flowing through a larger exterior conduit. The devices include an inline fluid damper device that is placed inside of the larger exterior conduit. The damper device includes one or more interior conduits that divide the fluid that is flowing through the exterior conduit into one or more portions. The divided fluid flows along a center axis and in one or more different directions along one or more flow paths created by the interior conduits. One technical effect of the subject matter described herein is improved reduction of fluid pressure or flow fluctuations responsive to mechanical vibrations caused by the engine assembly in operation. For example, the systems and methods described herein may improve the reduction of fuel line pressure fluctuations or fuel line flow fluctuations in the fluid responsive to the fluid being unsteady or responsive to the engine assembly creating and/or causing mechanical vibrations, or the like.
-
FIG. 1 illustrates anassembly 10 in accordance with one embodiment. Thesystem 10 includes anexterior conduit 54 that is coupled between asystem 12 and areservoir 52. Theexterior conduit 54 is a conduit (e.g., channel, tube, hose, pipe, or the like) that delivers fluid from thereservoir 52 to thesystem 12. For example, theexterior conduit 54 may be a fuel line and thesystem 12 may be an engine system. Theexterior conduit 54 may provide the passage of fuel from thereservoir 52 to a combustor of the engine system. Optionally, thesystem 12 may be any alternative mechanical system and theexterior conduit 54 may pass any fluid between thereservoir 52 and thesystem 12. Theexterior conduit 54 may be rigid, flexible, or a combination of rigid and flexible along the length of theexterior conduit 54 between thereservoir 52 and thesystem 12. Optionally, pluralexterior conduits 54 may be operably coupled with thereservoir 52, thesystem 12, an alternative reservoir (not shown), a second system, another component, or any combination therein. - An inline
fluid damper device 100 is disposed inside theexterior conduit 54 at a location between thereservoir 52 and thesystem 10. For example, the inlinefluid damper device 100 is located upstream of thesystem 10. Theexterior conduit 54 may be referred to as a largerexterior conduit 54 such that the largerexterior conduit 54 has a cross-sectional area that is larger relative to the size and/or shape of thedamper device 100. For example, thedamper device 100 is sized and shaped in order to be entirely contained within the largerexterior conduit 54. In the illustrated embodiment, thedamper device 100 is disposed at a position that is closer to thereservoir 52 than thesystem 12. Optionally, thedamper device 100 may be disposed at any location between thereservoir 52 and thesystem 12. Additionally or alternatively, one ormore damper devices 100 may be disposed inside of the largerexterior conduit 54. For example, afirst damper device 100 may be disposed closer to thereservoir 52 and a second damper device may be disposed closer to thesystem 12 such that the fluid sequentially flows through the first damper device then the second damper device between thereservoir 52 and thesystem 12. Optionally, one ormore damper devices 100 may be disposed inside of thefuel line 54 at any location, in any configuration, or the like. Thedamper device 100 is configured to substantially fill an interior chamber of the largerexterior conduit 54. Optionally, thedamper device 100 may not substantially fill the interior chamber of the largerexterior conduit 54. -
FIG. 2 illustrates a perspective view of the inlinefluid damper device 100 in accordance with one embodiment. Thedamper device 100 includes one or more interior conduits that are placed inside of the largerexterior conduit 54. In the illustrated embodiment ofFIG. 2 , the inlinefluid damper device 100 includes two 204, 210. Theinterior conduits interior conduit 204 may be referred to herein as a flow-throughconduit 204, and theinterior conduit 210 may be referred to as anindirect flow conduit 210. Optionally, thedamper device 100 may include plural flow-throughconduits 204 and/or pluralindirect flow conduits 210. - The flow-through
conduit 204 extends a length L between afirst end 206 and asecond end 208. The flow-throughconduit 204 is a channel or passage through which fluid flows between thefirst end 206 and thesecond end 208. Additionally or alternatively, thedamper device 100 may include two or more flow-throughconduits 204 through which fluid flows between the first and second ends 206, 208. The flow-throughconduit 204 is elongated along and extends around acenter axis 202. In the illustrated embodiment, the flow-throughconduit 204 is substantially centered about thecenter axis 202 between the first and second ends 206, 208. Optionally, the flow-throughconduit 204 may not be centered about thecenter axis 202 along the length L. Additionally or alternatively, the flow-throughconduit 204 may extend along a different axis. For example, the flow-throughconduit 204 may be substantially centered about thecenter axis 202 at a position near thefirst end 206, and may not be substantially centered about thecenter axis 202 at a position near thesecond end 208. Additionally or alternatively, the flow-throughconduit 204 may extend along a different axis that is substantially parallel with thecenter axis 202. - In the illustrated embodiment, the flow-through
conduit 204 has a substantially circular cross-sectional shape and is tubular between the first and second ends 206, 208. Optionally, the flow-throughconduit 204 may have any alternative cross-sectional shape such as, but not limited to, quadrilateral, oval, or the like. Optionally, the flow-throughconduit 204 may have one or more different and/or varying cross-sectional shapes along the length L between thefirst end 206 and thesecond end 206. For example, theconduit 204 may have a circular cross-sectional shape at a position near thefirst end 206 and may have a quadrilateral cross-sectional shape at a position near thesecond end 208, may have a circular cross-sectional shape near thefirst end 206 and a concentric smaller or larger circular cross-sectional shape near thesecond end 208, or the like. - The
indirect flow conduit 210 is operably coupled with the flow-throughconduit 204 and disposed outside of the flow-throughconduit 204. Theindirect flow conduit 210 extends a length SL along thecenter axis 202. In the illustrated embodiment, the length SL is less than the length L of the flow-throughconduit 204. Additionally or alternatively, the length SL may be substantially equal to the length L. Theindirect flow conduit 210 may begin substantially at or near thefirst end 206, may end substantially at or near thesecond end 208, or a combination therein. - The
indirect flow conduit 210 includes aspiral protrusion 216 that is helically wrapped around the flow-throughconduit 204. Thespiral protrusion 216 radially protrudes from the flow-throughconduit 204 away from thecenter axis 202. For example, thespiral protrusion 216 protrudes away from the flow-throughconduit 204 in a radial direction generally perpendicular to or otherwise away from thecenter axis 202. Optionally, one or more of the spirals of the spiral protrusion may extend in any direction away from the flow-throughconduit 204. - In the illustrated embodiment, the
spiral protrusion 216 is helically wrapped seventeen times around the flow-throughconduit 204 and each protrusion is disposed equidistance apart from each other along the length SL. Optionally, thespiral protrusion 216 may include any number of helically wrapped spirals. Additionally or alternatively, any number of the spiral protrusions may be positioned equidistance or non-equidistance apart from each other along the length SL. Additionally, each spiral extends substantially equal distances radially away from the flow-throughconduit 204. Optionally, one or more of the spirals may extend a distance less than or greater than one or more alternative spirals. - In the illustrated embodiment, the
spiral protrusion 216 extends the length SL that is less than the length L of the flow-throughconduit 204. For example, thespiral protrusion 216 is helically wrapped around the flow-throughconduit 204 at least partially between thefirst end 206 and thesecond end 208 of the flow-throughconduit 204 along thecenter axis 202. Optionally, thespiral protrusion 216 may be helically wrapped around the flow-through conduit 204 a length that is substantially equal to the length L between the first and second ends 206, 208. In the illustrated embodiment, thespiral protrusion 216 extends a continuous length along the length SL of theindirect flow conduit 210. Additionally or alternatively, one or morespiral protrusions 216 may extend one or more common and/or unique non-continuous lengths. Optionally, one or morespiral protrusions 216 may have any alternative configuration. - The
damper device 100 is a unitary device that includes the flow-throughconduit 204 integrally formed with theindirect flow conduit 210 as a single device manufactured of a common material. For example, thedamper device 100, including the flow-throughconduit 204 and theindirect flow conduit 210, may be die-cast, injection molded, machined, or the like. Additionally or alternatively, one or more of the interior conduits (e.g., the flow-throughconduit 204 or the indirect flow conduit 210) may be formed as separate components. For example, theindirect flow conduit 210 may be welded to, printed on, mechanically fastened to, or the like, the flow-throughconduit 204. Additionally or alternatively, the flow-throughconduit 204 may be manufactured out of a material that is unique to the material of theindirect flow conduit 210. Optionally, the damper device may be manufactured by any alternative methods. Thedamper device 100 and/or one or more of the flow-throughconduit 204 or theindirect flow conduit 210 may be manufactured of a metallic alloy or a non-metallic material. Optionally, thedamper device 100 may be a flexible or rigid device. For example, thedamper device 100 may be flexible such that thedevice 100 may flex in order to conform to the largerexterior conduit 54. -
FIG. 3 illustrates a cross-sectional view of the inlinefluid damper device 100 that is disposed inside of the largerexterior conduit 54 in accordance with one embodiment. Thespiral protrusion 216 radially protrudes 310, 312 between the flow-throughdistances conduit 204. For example, thespiral protrusion 216 is operably coupled with the flow-throughconduit 204 at anouter surface 304 of the flow-throughconduit 204. Thespiral protrusion 216 extends 310, 312 from thedistances outer surface 304 of the flow-throughconduit 204 to aninner surface 306 of the largerexterior conduit 54. In the illustrated embodiment ofFIG. 3 , the flow-throughconduit 204 is generally centered about thecenter axis 202, and thespiral protrusion 216 radially protrudes away from the flow-throughconduit 204. Additionally or alternatively, thedistance 310 may be greater than (e.g., a larger distance) or less than (e.g., a shorter distance) than thedistance 312 between theouter surface 304 and theinner surface 306. For example, the flow-throughconduit 204 and thespiral protrusion 216 may not be generally centered about thecenter axis 202. - Referring to
FIGS. 2 and 3 , thedamper device 100 placed inside of the largerexterior conduit 54 divides the fluid that is flowing in a direction A from thereservoir 52 into afirst portion 212 and asecond portion 214. Thefirst portion 212 of the fluid flows along thecenter axis 202 through the flow-throughconduit 204 from thefirst end 206 to thesecond end 208. Optionally, thefirst portion 212 may flow in a direction from thesecond end 208 to thefirst end 206. Thesecond portion 214 of the fluid flows outside of the flow-throughconduit 204 along thecenter axis 202 and along a different direction. For example, thesecond portion 214 of the fluid flows in a direction around thespiral protrusion 216 of theindirect flow conduit 210 along thecenter axis 202. The first and 212, 214 of the fluid may contain substantially the same or substantially different volumes of the fluid. For example, the flow-throughsecond portions conduit 204 may be sized and shaped such that the flow-throughconduit 204 may allow more or less fluid (e.g., a larger or smaller volume of fluid) to be divided into thefirst portion 212 relative to thesecond portion 214. - The
first portion 212 of the fluid flows through the flow-throughconduit 204 concurrently with thesecond portion 214 of the fluid that flows outside of the flow-through conduit 204 (e.g., along the path created by the indirect flow conduit 210), respectively. For example, the fluid flowing in the direction A that is divided into the first and 212, 214 flows through the flow-throughsecond portions conduit 204 and outside of the flow-through conduit 204 (e.g., along the flow path of the indirect flow conduit 210) at substantially the same time. Additionally, theindirect flow conduit 210 creates a longer flow path for thesecond portion 214 of the fluid to flow from thefirst end 206 to thesecond end 208 relative to the flow path created by the flow-throughconduit 204 for thefirst portion 212 of the fluid to flow from thefirst end 206 to thesecond end 208. For example, the time it takes for thesecond portion 214 of the fluid to flow along the path created by theindirect flow conduit 210 is longer (e.g., a larger or greater amount of time) relative to the time it takes for thefirst portion 212 of the fluid to concurrently flow (e.g., flow at substantially the same time) along the path created by the flow-throughconduit 204. -
FIG. 4 illustrates a perspective view of an inlinefluid damper device 400 in accordance with one embodiment. Thedamper device 400 includes arod 420 and aninterior conduit 410. Theinterior conduit 410 may be referred to herein as anindirect flow conduit 410. Therod 420 extends a length L between afirst end 406 and asecond end 408 along thecenter axis 202. Theindirect flow conduit 410 extends a length SL along thecenter axis 202. In the illustrated embodiment, the length SL is less than the length L of therod 420. Additionally or alternatively, the length SL may be substantially equal to the length L. Theindirect flow conduit 410 may begin substantially at thefirst end 406, may end substantially at thesecond end 408, or a combination therein. - The
indirect flow conduit 410 includes aspiral protrusion 416 that is helically wrapped around therod 420. In the illustrated embodiment, thespiral protrusion 416 is helically wrapped seventeen times around therod 420 and each protrusion is disposed equidistance apart from each other protrusion along the length SL. Optionally, thespiral protrusion 416 may include any number of helically wrapped spirals that are spaced any uniform and/or non-uniform distances apart from each other. In the illustrated embodiment, each spiral of thespiral protrusion 416 radially protrudes a common distance away from anexterior surface 424 of therod 420. For example, each spiral of thespiral protrusion 416 extends radially away from thecenter axis 202 between theexterior surface 424 and an inner surface of the larger exterior conduit 54 (e.g., inner surface 306). Optionally, one or more spirals may not extend to the inner surface of theexterior conduit 54. - The
damper device 400 is placed inside of the largerexterior conduit 54 and directs the fluid that is flowing in a direction A from the reservoir into aportion 414. Theportion 414 of the fluid flows outside of therod 420 along thecenter axis 202 and in a direction around thespiral protrusion 416 of theindirect flow conduit 410 along thecenter axis 202. Thespiral protrusion 416 of theindirect flow conduit 410 creates a longer flow path for theportion 414 of the fluid to flow from thefirst end 406 to thesecond end 408 relative to a flow path that is devoid thespiral protrusion 416. For example, theindirect flow conduit 410 of thedamper device 400 creates a flow path for the fluid to flow such that the fluid flowing in the direction A flows slower along the flow path created by theindirect flow conduit 410 relative to the flow of the fluid outside of theindirect flow conduit 410 and inside of the larger exterior conduit 54 (e.g., before and/or after the fluid flows through the indirect flow conduit 410). Additionally or alternatively, thespiral protrusion 416 of theindirect flow conduit 410 may be shaped and/or sized in order to change the speed of the fluid that flows through thedamper device 400. -
FIG. 5 illustrates a perspective view of an inlinefluid damper device 500 in accordance with one embodiment. Thedamper device 500 includes 504, 510A, 510B. Theinterior conduits interior conduit 504 may be referred to herein as a flow-throughconduit 504, theconduit 510A may be referred to herein as a firstindirect flow conduit 510A, and theconduit 510B may be referred to herein as a secondindirect flow conduit 510B. The flow-throughconduit 504 extends a length L between afirst end 506 and asecond end 508 along thecenter axis 202. The first and second 510A, 510B are operably coupled with the flow-throughindirect flow conduits conduit 504 and are disposed outside of the flow-throughconduit 504. The firstindirect flow conduit 510A extends a length SL-A along thecenter axis 202 and the secondindirect flow conduit 510B extends a length SL-B along thecenter axis 202. In the illustrated embodiment, the length SL-A is substantially equal to the length SL-B. Optionally, the firstindirect flow conduit 510A may extend a length SL-A that may be less than or greater than the length SL-B of the secondindirect flow conduit 510B. Additionally, the lengths SL-A, SL-B are separated by adistance 522 in a direction along thecenter axis 202. Optionally, the lengths SL-A, SL-B may be separated by a distance greater than or less than thedistance 522. - The first and second
510A, 510B includeindirect flow conduits 516A, 516B, respectively, that are helically wrapped around the flow-throughspiral protrusions conduit 504. For example, the 516A, 516B radially protrude from anspiral protrusions outer surface 524 of the flow-throughconduit 504 away from thecenter axis 202. In the illustrated embodiment, thespiral protrusion 516A of the firstindirect flow conduit 510A is helically wrapped five times around the flow-throughconduit 504, and thespiral protrusion 516B of the secondindirect flow conduit 510B is helically wrapped five times around the flow-throughconduit 504. Optionally, the first and/or second 510A, 510B may include less than five or more than five spirals wrapped around the flow-throughindirect flow conduits conduit 504. - The
damper device 500 placed inside of the largerexterior conduit 54 divides the fluid that is flowing in the direction A into afirst portion 512 and a second portion 514. Thefirst portion 512 flows along thecenter axis 202 through the flow-throughconduit 504 between thefirst end 506 and thesecond end 508. The second portion 514 flows outside of the flow-throughconduit 504 along thecenter axis 202 and along a different direction. For example, the second portion 514 flows in a direction around the spiral protrusions 516 of the first and second 510A, 510B. For example, the second portion 514 of the fluid flows along the flow path created by theindirect flow conduits spiral protrusion 516A of the firstindirect flow conduit 510A and then along the flow path created by thespiral protrusion 516B of the secondindirect flow conduit 510B. - In the illustrated embodiment, the flow paths created by the spiral protrusions 516 of the first and second
510A, 510B rotatably extend in a common direction around the center axis 202 (e.g., in a clockwise direction). Optionally, the spiral protrusions of the first and/or secondindirect flow conduits 510A, 510B may create a flow path that flows in a unique direction around theindirect flow conduits center axis 202. For example, thesecond portion 514A of the fluid may first flow in a clockwise direction around thespiral protrusion 516A of the firstindirect flow conduit 510A and then thesecond portion 514B may flow in a counter-clockwise direction around thespiral protrusion 516B of the secondindirect flow conduit 510B, or any alternative combination therein. Additionally or alternatively, thedamper device 500 may include more than two indirect flow conduits 510 that may direct the second portion 514 of the fluid to flow in any direction. - The
first portion 512 of the fluid flows through the flow-throughconduit 504 concurrently with the second portion 514 of the fluid that flows outside of the flow-through conduit 504 (e.g., along the path created by the first and second 510A, 510B). For example, the fluid flowing in the direction A that is divided into the first andindirect flow conduits second portions 512, 514 flows along the flow paths created by the flow-throughconduit 504 and the first and second 510A, 510B at substantially the same time. Additionally, the first and secondindirect flow conduits 510A, 510B create a longer flow path for the second portion 514 of the fluid to flow from theindirect flow conduits first end 506 to thesecond end 508 relative to the flow path created by the flow-throughconduit 504 for thefirst portion 512 of the fluid to flow from thefirst end 506 to thesecond end 508. For example, the time it takes for the second portion 514 of the fluid to flow along the flow path created by the 510A, 510B is longer (e.g., a larger or greater amount of time) relative to the time it takes for theindirect flow conduits first portion 512 of the fluid to concurrently flow along the flow path created by the flow-throughconduit 504. -
FIG. 6 illustrates a perspective view of an inlinefluid damper device 600 in accordance with one embodiment. Thedamper device 600 includes 604 and 610. Theinterior conduits interior conduit 604 may be referred to herein as a flow-throughconduit 604, and theinterior conduit 610 may be referred to herein as anindirect flow conduit 610. The flow-throughconduit 604 is elongated along and generally centered about thecenter axis 202 between first and second ends 606, 608. Optionally, the flow-throughconduit 604 may not be generally centered about thecenter axis 202, thedamper device 600 may include two or more flow-throughconduits 604 that may be operably coupled with each other flow-throughconduit 604 and may be elongated along thecenter axis 202, or any combination therein. Theindirect flow conduit 610 is operably coupled with the flow-throughconduit 604 and disposed outside of the flow-throughconduit 604. Optionally, two or moreindirect flow conduits 610 may be operably coupled with and disposed outside of the flow-throughconduit 604. - The
indirect flow conduit 610 includes aspiral protrusion 616 that is helically wrapped around the flow-throughconduit 604. For example, thespiral protrusion 616 radially protrudes from anouter surface 624 of the flow-throughconduit 604 away from thecenter axis 202. Thespiral protrusion 616 includesplural baffles 622 that are disposed along the length SL of theindirect flow conduit 610. Thebaffles 622 extend between and operably couple two or more of the spirals of thespiral protrusion 616 along the length SL. For example, thebaffles 622 may be referred to as steps or plates that protrude in a direction generally parallel to the elongated direction of thedamper device 600. Optionally, thebaffles 622 may protrude in any direction between two or more spirals. - The
damper device 600 placed inside of the largerexterior conduit 54 divides the fluid that is flowing in the direction A into afirst portion 612 and asecond portion 614. The first portion flows along thecenter axis 202 through the flow-throughconduit 604. Thesecond portion 614 flows outside of the flow-throughconduit 604 and along a flow path that is created by thebaffles 622 and spirals of thespiral protrusion 616 of theindirect flow conduit 610. Theindirect flow conduit 610 creates a longer flow path for thesecond portion 614 of the fluid to flow from thefirst end 606 to thesecond end 608 relative to the flow path created by the flow-throughconduit 604 for thefirst portion 612 of the fluid to flow from thefirst end 606 to thesecond end 608. For example, the time is takes for thesecond portion 614 of the fluid to flow along the flow path created by theindirect flow conduit 610 is longer (e.g., a larger or greater amount of time) relative to the time it takes for thefirst portion 612 of the fluid to concurrently flow along the flow path created by the flow-throughconduit 604. -
FIG. 7 illustrates a cross-sectional perspective view of an inlinefluid damper device 700 in accordance with one embodiment. Thedamper device 700 includes 704 and 710. Theinterior conduits interior conduit 704 may be referred to herein as a flow-throughconduit 704, and theinterior conduit 710 may be referred to herein as anindirect flow conduit 710. The flow-throughconduit 704 is elongated along and generally centered about thecenter axis 202 between first and second ends 706, 708. The flow-throughconduit 704 includes aninner surface 726 and anouter surface 724. The flow-throughconduit 704 includes arod 720 that is elongated along and is generally centered about thecenter axis 202. In the illustrated embodiment, therod 720 is a solid or closed rod. Optionally, therod 720 may be an open passage or channel between thefirst end 706 and thesecond end 708. - The flow-through
conduit 704 also includes aninner spiral protrusion 728 that is operably coupled with theinner surface 726 of the flow-throughconduit 704. Theinner spiral protrusion 728 is helically wrapped around therod 720 between the first and second ends 706, 708. In the illustrated embodiment, theinner spiral protrusion 728 includes five spirals that are disposed substantially equidistance apart from each other. Optionally, theinner spiral protrusion 728 may include any number of spirals, the spirals may be spaced apart any common or unique distances, the spirals may have a multi-spiral counter-rotating configuration, may have a multi-spiral co-rotating configuration, or any combination therein. - The
indirect flow conduit 710 is operably coupled with theouter surface 724 of the flow-through conduit and is disposed outside of the flow-throughconduit 704. Optionally, two or moreindirect flow conduits 710 may be operably coupled with and disposed outside of the flow-throughconduit 704. Theindirect flow conduit 710 includes aspiral protrusion 716 that is helically wrapped around the flow-throughconduit 704. For example, thespiral protrusion 716 radially protrudes from theouter surface 724 of the flow-throughconduit 704 away from thecenter axis 202. - The
damper device 700 placed inside of the largerexterior conduit 54 divides the fluid into afirst portion 712 and asecond portion 714. Thefirst portion 712 flows through the flow-throughconduit 704 and along the flow path created by therod 720 and theinner spiral protrusion 728. For example, thefirst portion 712 of the fluid flows through the flow-throughconduit 704 along thecenter axis 202 in a rotating counter-clockwise direction from thefirst end 706 to thesecond end 708. Thesecond portion 714 flows outside of the flow-throughconduit 704 and along a flow path that is created by the spirals of thespiral protrusion 716. For example, thesecond portion 714 of the fluid flows outside of the flow-throughconduit 704 along thecenter axis 202 in a rotating clockwise direction from thefirst end 706 to thesecond end 708. Additionally or alternatively, theinner spiral protrusion 728 and thespiral protrusion 716 may be helically wrapped around the flow-throughconduit 704 such that thefirst portion 712 of the fluid and thesecond portion 714 of the fluid flow in the same rotating direction from thefirst end 706 to thesecond end 708. For example, theinner spiral protrusion 728 may be shaped in order to create a flow path for thefirst portion 712 of the fluid to flow in a same rotating direction as the flow path for thesecond portion 714 that is created by thespiral protrusion 716. - In the illustrated embodiment, the
spiral protrusion 716 of theindirect flow conduit 710 is shaped and/or sized in order to create a longer flow path for thesecond portion 714 of the fluid to flow from thefirst end 706 to thesecond end 708 relative to flow path created by theinner spiral protrusion 728 of the flow-throughconduit 704 for thefirst portion 712 of the fluid to concurrently flow from thefirst end 706 to thesecond end 708. Optionally, theinner spiral protrusion 728 and/or therod 720 of the flow-throughconduit 704 may be shaped and/or sized in order to create a longer flow path for thefirst portion 712 for the fluid to flow relative to thesecond portion 714 of the fluid. Optionally, theinner spiral protrusion 728 may be shaped and/or sized in order to create a flow path for thefirst portion 712 that has a length that is substantially the same as a length of the flow path created by thespiral protrusion 716 of theindirect flow conduit 710. For example, the flow-throughconduit 704 and theindirect flow conduit 710 may be shaped/sized in order for the first and 712, 714 of the fluid to concurrently flow through thesecond portions damper device 700 in substantially the same amount of time or in different amounts of time. -
FIG. 8 is a cross-sectional perspective view of an inlinefluid damper device 800 in accordance with one embodiment. Thedamper device 800 includes aninterior conduit 804. Theinterior conduit 804 may be referred to as a flow-throughconduit 804. The flow-throughconduit 804 is elongated along thecenter axis 202 between first and second ends 806, 808. The flow-throughconduit 804 includes aninner surface 826 and anouter surface 824. - The
damper device 800 includes aplate 820 that is disposed inside of the flow-throughconduit 804. Theplate 820 is elongated along and generally centered about thecenter axis 202. Theplate 820 extends between afirst end 842 that is disposed near thefirst end 806 of the flow-throughconduit 804 and asecond end 844 that is disposed near thesecond end 806 of the flow-throughconduit 804. In the illustrated embodiment, theplate 820 extends a distance between the first and second ends 842, 844 that is shorter than the length of the flow-throughconduit 804. Optionally, theplate 820 may extend a length that is substantially the same length as the flow-throughconduit 804. Additionally, thefirst end 842 includes afirst end baffle 852 and thesecond end 844 includes asecond end baffle 854. The first and second end baffles 852, 855 protrude a distance away from theplate 820 in a direction generally away from thecenter axis 202. - The
plate 820 divides the flow-throughconduit 804 into a first flow-throughconduit 804A and a second flow-throughconduit 804B that is substantially equal in shape and size with the first flow-throughconduit 804A between the first and second ends 806, 808. For example, the first and second flow-through 804A, 804B may have substantially the same volume inside of theconduits damper device 800. Optionally, theplate 820 may not be generally centered about thecenter axis 202 such that the first and second flow-through 804A, 804B are not substantially equal in shape or size. Additionally or alternatively, theconduits damper device 800 may include any number ofplates 820 that may divide the flow-throughconduit 804 into any number of divided flow-through conduits. Theplate 820 has afirst side 834 and an oppositesecond side 836. For example, thefirst side 834 faces the first flow-throughconduit 804A, and thesecond side 836 faces towards the second flow-throughconduit 804B. - The
damper device 800 includes one or more exterior baffles 822 that are operably coupled with theinner surface 826 of the flow-throughconduit 804. The baffles 822 protrude a distance away from theinner surface 826 of the flow-throughconduit 804 and in a direction towards thecenter axis 202. In the illustrated embodiment, the exterior baffles 822 extend a distance away from theinner surface 826 in a direction generally perpendicular to thecenter axis 202. Optionally, one or more of the exterior baffles 822 may extend in any common or unique direction away from theinner surface 826. The first flow-throughconduit 804A includes fiveexterior baffles 822A and the second flow-throughconduit 804B includes eightexterior baffles 822B. Additionally or alternatively, the first or second flow-through 804A, 804B may include any number of exterior baffles 822.conduits - The
plate 820 includes one or more interior baffles 832 that are operably coupled with theplate 820 and protrude a distance away from theplate 820 in a direction generally away from theplate 820. In the illustrated embodiment, theplate 820 includes fourinterior baffles 832A that are operably coupled with thefirst side 834 of theplate 820. The fourinterior baffles 832A extend a common distance away from thefirst side 834 of theplate 820 and protrude into the first flow-throughconduit 804A. Additionally, in the illustrated embodiment, theplate 820 includes seveninterior baffles 832B that are operably coupled with thesecond side 836 of theplate 820. The seveninterior baffles 832B extend a common distance away from thesecond side 836 of theplate 820 and protrude into the second flow-throughconduit 804B. Additionally or alternatively, any number of baffles 832 may extend away from the first or 834, 836 of thesecond sides plate 820 and protrude into the first or second flow-through 804A, 804B. The interior baffles 832 extend away from theconduits plate 820 in a direction substantially perpendicular to thecenter axis 202. Optionally, any number of baffles 832 may extend in any direction away from theplate 820. - The
damper device 800 placed inside of the largerexterior conduit 54 divides the fluid into afirst portion 812A and asecond portion 812B. Thefirst portion 812A flows through the first flow-throughconduit 804A and along the flow path created by the interior and 832A, 822A that protrude into the first flow-throughexterior baffles conduit 804A. Thesecond portion 812B of the fluid flows through the second flow-throughconduit 804B and along the flow path created by the interior and 832B, 822B that protrude into the second flow-throughexterior baffles conduit 804B. - In the illustrated embodiment, the second flow-through
conduit 804B includes more interior and 832B, 822A than the first flow-throughexterior baffles conduit 804A. For example, the second flow-throughconduit 804B is shaped and sized in order to create a longer flow path for thesecond portion 812B of the fluid to flow from thefirst end 806 to thesecond end 808 relative to the flow path created by the first flow-throughconduit 804A. Additionally or alternatively, the first and second flow-through 804A, 804B may include a common number of interior and/or exterior baffles 832, 822 such that the first and second flow-throughconduits 804A, 804B create a substantially common flow path for the first andconduits 812A, 812B of the fluid to flow.second portions -
FIGS. 2 through 8 illustrate six embodiments of inline fluid damper devices. - Additionally or alternatively, one or more features or components of the damper devices illustrated in
FIGS. 2 through 8 may be combined in any combination, configuration, or the like. Optionally, an inline damper device may have any alternative shape, size, configuration, or the like, of one or more flow-through conduits, one or more indirect flow conduits, one or more portions of fluid flowing along one or more flow paths, or the like. In one embodiment, a dampening system is provided that includes any two or more of the damper devices described herein (the same or different embodiments of the devices) disposed back-to-back or otherwise in a serial relationship such that fuel or other fluids sequentially flow through the multiple damper devices between a fluid reservoir and a load (e.g., an engine). -
FIG. 9 is a translucent perspective view of an inlinefluid damper device 1000 in accordance with one embodiment. Thedamper device 1000 includes 1004, 1010A, 1010B. Theinterior conduits interior conduit 1004 may be referred to herein as a flow-throughconduit 1004, theinterior conduit 1010A may be referred to herein as a firstindirect flow conduit 1010A, and theinterior conduit 1010B may be referred to herein as a secondindirect flow conduit 1010B. The flow-throughconduit 1004 is elongated along thecenter axis 202 between first and 1006, 1008. The flow-throughsecond ends conduit 1004 includes aninner surface 1026 and anouter surface 1024. - The first and second
1010A, 1010B include one or more closed loops 1022 that radially protrude from the flow-throughindirect flow conduits conduit 1004 in a direction away from thecenter axis 202. Each of the closed loops 1022 includes a loop baffle 1020 that is disposed inside of each of the closed loops 1022. For example, the loop baffles 1020 separate the closed loops 1022 of the first and second 1010A, 1010B from the flow-throughindirect flow conduits conduit 1004. - In the illustrated embodiment, the first
indirect flow conduit 1010A includes threeclosed loops 1022A that radially protrude from the flow-throughconduit 1004 on a first side of thecenter axis 202, and the secondindirect flow conduit 1010B includes fourclosed loops 1022B that radially protrude from the flow-throughconduit 1004 on an opposite, second side of thecenter axis 202. Additionally or alternatively, thedamper device 1000 may include any number of indirect flow conduits 1010 that may include any number of closed loops 1022 that may protrude from any side of thecenter axis 202. - The
1022A, 1022B are arranged in an alternating configuration along the length of theclosed loops damper device 1000 between the first and 1006, 1008. Optionally, the first and secondsecond ends 1010A, 1010B may include any common or unique number of closed loops 1022. Additionally or alternatively, the closed loops 1022 of the first and secondindirect flow conduits 1010A, 1010B may be arranged in any alternating, random, patterned, continuous configuration, or the like, between the first andindirect flow conduits 1006, 1008. For example, the firstsecond ends indirect flow conduit 1010A may include one or moreclosed loops 1022A that may protrude from the flow-throughconduit 1004 on the first side of thecenter axis 202, and the secondindirect flow conduit 1010B may not include anyclosed loops 1022B that protrude from the flow-throughconduit 1004. Optionally, the closed loops 1022 and the first and second 1010A, 1010B may have any alternative configuration.indirect flow conduits - The
damper device 1000 placed inside of the largerexterior conduit 54 divides the fluid flowing in the direction A into afirst portion 1012, asecond portion 1014A, and athird portion 1014B. Thefirst portion 1012 of the fluid flows through the flow-throughconduit 1004 from thefirst end 1006 to thesecond end 1008. Thesecond portion 1014A of the fluid flows through the firstindirect flow conduit 1010A and around theclosed loops 1022A of the firstindirect flow conduit 1010A. Thethird portion 1014B of the fluid flows through the secondindirect flow conduit 1010B and around theclosed loops 1022B of the secondindirect flow conduit 1010B. For example, the loop baffles 1020A of the firstindirect flow conduit 1010A directs the flow of thesecond portion 1014A of the fluid around the loop baffles 1020A and around theclosed loops 1022A. Additionally, the loop baffles 1020B of the secondindirect flow conduit 1010B directs the flow of thethird portion 1014B of the fluid around the loops baffles 1020B and around theclosed loops 1022B. - The
1022A, 1022B of the first and secondclosed loops 1010A, 1010B create a longer flow path for theindirect flow conduits second portion 1014A and thethird portion 1014B of the fluid to flow from thefirst end 1006 to thesecond end 1008 relative to the flow path created by the flow-throughconduit 1004. For example, thefirst portion 1012 of the fluid that flows through the flow path created by the flow-throughconduit 1004 flows from thefirst end 1006 to thesecond end 1008 more quickly (e.g., in a shorter amount of time) than the second and 1014A, 1014B of the fluid that flow through the flow paths created by the first and secondthird portions 1010A, 1010B, respectively.indirect flow conduits -
FIG. 10A illustrates a perspective view of an inlinefluid damper device 1200 in accordance with one embodiment.FIG. 10B illustrates a front view of the inlinefluid damper device 1200.FIGS. 10A and 10B will be discussed together in detail. - The inline
fluid damper device 1200 includes plural elongated stems 1222 that are coupled with each other atplural nodes 1228. Thedamper device 1200 may be formed as a unitary damper device and/or as a multiple component damper device. For example, thedamper device 1200 may be cast as a single, unitary, monolithic device including plural stems that are cast or formed together. Optionally, the stems may be welded, adhered, clipped, fastened, or the like, with each other at thenodes 1228. Optionally, at least part of thedamper device 1200 may be formed as a unitary damper device and one or more stems 1222 may be operably coupled with the at least part unitary damper device. In the illustrated embodiment, the stems 1222 are arranged in a repeating lattice pattern. For example, the stems 1222 are substantially uniform in shape and size and are arranged such that the stems 1222 form plural cells that are substantially uniformly spaced apart between the stems 1222. Optionally, thedamper device 1200 may include any number ofstems 1222 that may be arranged in any random and/or patterned configuration along the length of thedamper device 1200. For example, thedamper device 1200 may include any number ofstems 1222 of any unique and/or uniform shape and/or size that may be arranged in order to form any unique and/or uniform size of cells between the stems 1222. - The plural stems 1222 coupled with each other at the
plural nodes 1228 forms a flow-throughconduit 1204. The flow-throughconduit 1204 is elongated along and substantially centered about thecenter axis 202. The flow-throughconduit 1204 extends between afirst end 1206 and asecond end 1208. In the illustrated embodiment, the stems 1222 andnodes 1228 are shaped, sized, and arranged such that the flow-throughconduit 1204 is generally centered about thecenter axis 202. Additionally or alternatively, the stems 1222 andnodes 1228 may be arranged in any alternative configuration such that the flow-throughconduit 1204 may not be substantially centered about thecenter axis 202. - The
damper device 1200 placed inside of the largerexterior conduit 54 divides the fluid flowing in the direction A such that at least some of the fluid flows through the flow-throughconduit 1204 without contacting any stems 1222 and/ornodes 1228 and at least some of the fluid concurrently flows through the flow-throughconduit 1204 and contacts one or more of thestems 1222 and/ornodes 1228. For example, at least some of the fluid flows in adirection 1212 along thecenter axis 202 and through the flow-throughconduit 1204 such that the fluid that flows in thedirection 1212 does not contact, touch, interact with, or the like, with any of thestems 1222 and/ornodes 1228. Additionally, at least some of the fluid flows in adirection 1214 such that the fluid that flows in thedirection 1214 does contact, touch, interact with, or the like, one or more of thestems 1222 and/or one or more of thenodes 1228. The stems 1222 coupled at thenodes 1228 create a flow path for the fluid that is flowing in the direction 1214 (e.g., the fluid that contacts thestems 1222 and nodes 1228) that is longer relative to a flow path created by thestems 1222 andnodes 1228 for the fluid that is flowing in the direction 1212 (e.g., the fluid that does not contact the stems 1222 or nodes 1228). For example, the one or more stems 1222 and/or the one ormore nodes 1228 may create or increase frictional drag as the fluid flows along the flow path in thedirection 1214 and contacts thestems 1222 and/ornodes 1228 relative to the at least some of the fluid that flows along the flow path that does not contact the stems 1222 and/or nodes 1228 (e.g., the fluid that flows in the direction 1212). -
FIG. 11A illustrates a perspective view of an inlinefluid damper device 1300 in accordance with one embodiment.FIG. 11B illustrates a front view of the inlinefluid damper device 1300.FIGS. 11A and 11B will be discussed together in detail. - The
damper device 1300 includes plural elongated stems 1322 that are coupled with each other atplural nodes 1328. Thedamper device 1300 may be formed as a unitary damper device and/or as a multiple component damper device. For example, thedamper device 1300 may be cast as a single, unitary, monolithic device including plural stems that are cast or formed together. Optionally, the stems 1322 may be welded, adhered, clipped, fastened, or the like, with each other at thenodes 1328. Optionally, at least part of thedamper device 1300 may be formed as a unitary damper device and one or more stems 1322 may be operably coupled with the at least part unitary damper device. In the illustrated embodiment, the stems 1322 are arranged in a random configuration. For example, the stems 1322 andnodes 1328 are arranged such that the stems 1322 form plural cells that are of random shape, random size, random distances apart, or the like, between the stems 1322. Optionally, thedamper device 1322 may include any number ofstems 1322 that are of any uniform or unique shape and/or size that may be arranged in order to form any uniform and/or unique size of cells between the stems 1322. - The plural stems 1322 coupled with each other at the
plural nodes 1328 forms anindirect flow conduit 1310. Theindirect flow conduit 1310 is elongated along and substantially centered about thecenter axis 202. Theindirect flow conduit 1310 extends between afirst end 1306 and asecond end 1308 along thecenter axis 202. In the illustrated embodiment, the stems 1322 andnodes 1328 are arranged such that one or more of thestems 1322 and one or more of thenodes 1328 intersect with theindirect flow conduit 1310 along thecenter axis 202. For example, one or more of thestems 1322 protrude distances away from thenodes 1328 such that one or more stems 1322 extend in one or more directions that may be substantially parallel to, may be substantially perpendicular to, may be non-parallel with, may be non-perpendicular with, or the like, thecenter axis 202. For example, one or more stems 1322 ornodes 1328 may intersect with thecenter axis 202 at one or more locations along thecenter axis 202 between thefirst end 1306 and thesecond end 1308. - The
damper device 1300 placed inside of the largerexterior conduit 54 divides the fluid flowing in the direction A such that the fluid flows through theindirect flow conduit 1310 and contacts one or more of thestems 1322 and/ornodes 1328. For example, at least some of the fluid flows from thefirst end 1306 to thesecond end 1308 and contacts, touches, interacts with, or the like, one or more of thestems 1322 and/or one or more of thenodes 1328. The stems 1322 coupled with each other at thenodes 1328 creates plural flow paths for the fluid that is flowing in the direction A such that the fluid may contact, touch, interact with, or the like, one or more stems 1322 and/or one ormore nodes 1328 as the fluid flows from thefirst end 1306 to thesecond end 1308. -
FIG. 12 illustrates aflowchart 1500 of a method in accordance with one embodiment. At 1502, an inline fluid damper device is placed inside of a larger exterior conduit through which a fluid is configured to flow. The damper device includes one or more interior conduits. The interior conduits may be elongated along and may extend around a center axis. For example, the damper device may include one or more flow-through conduits, one or more indirect flow conduits, a combination of one or more flow-through conduits and one or more indirect flow conduits, or the like. Optionally, the interior conduits may include one or more spiral protrusions, one or more closed loops, one or more baffles, one or more stems coupled with each other at one or more nodes, or any combination that may include any number of spiral protrusions, closed loops, baffles, stems, or the like. Additionally or alternatively, the interior conduits may have any alternative shape, size, orientation, or the like, that may divide the fluid that flows through the larger exterior conduit such that the fluid may flow the length of the damper device along any direction of a flow path created by the interior conduits. - At 1504, the fluid flows through the inline fluid damper device that is disposed inside of the larger exterior conduit. For example, the fluid may be fuel that flows through a fuel line to a gas turbine engine assembly. Optionally, the fluid may be a coolant that flows to a mechanical system, the fluid may be fuel that flows to any alternative mechanical system, the fluid may be any fluid that is removed from any mechanical system, or the like. The fluid flows through the larger exterior conduit and through the damper device, for example from a first end to a second end of the damper device. Additionally or alternatively, fluid may flow from the second end to the first end of the damper device. For example, fuel may be removed from the gas turbine engine assembly. Optionally, the larger exterior conduit may be any conduit operably coupled with any assembly through which a fluid may flow.
- At 1506, the one or more interior conduits of the damper device divides the fluid that flows through the damper device into one or more portions. For example, the damper device may include a single interior conduit, and the fluid may flow along a flow path created by the interior conduit. Optionally, the damper device may include two or more interior conduits. For example, the damper device may include a flow-through conduit (e.g., the flow-through
conduit 204 ofFIG. 2 ) and two indirect flow conduits (e.g., the indirect flow conduits 510 ofFIG. 5 ). The fluid may be divided into three portions such that a first portion may flow along a first flow path created by the flow-through conduit, a second portion may flow along a second flow path created by the first indirect flow conduit that is different from the first flow path, and a third portion may flow along a third flow path created by the second indirect flow conduit that is different from the first and second flow paths. Optionally, the fluid may be divided into any number of portions having substantially similar or substantially different volumes of the fluid. Additionally or alternatively, one or more of the interior conduits may be shaped and/or sized in order to create one or more flow paths having substantially similar flow paths. - In one embodiment of the subject matter described herein, an inline fluid damper device includes a flow-through conduit configured to be placed inside a larger exterior conduit through which a fluid flows. The flow-through conduit is elongated and extends around a center axis. The damper device also includes an indirect flow conduit coupled with the flow-through conduit. The indirect flow conduit is also configured to be placed inside the larger exterior conduit. The flow-through conduit and the indirect flow conduit are configured to dampen one or more flow fluctuations or pressure fluctuations in the fluid flowing in the larger exterior conduit by dividing the fluid into a first portion that flows along the center axis through the flow-through conduit and a second portion that concurrently flows outside of the flow-through conduit along the center axis and along a different direction.
- Optionally, the flow-through conduit is also configured to extend from a first end to a second end. The indirect flow conduit creates a longer flow path for the second portion of the fluid to flow from the first end to the second end relative to a flow path created by the flow-through conduit for the first portion of the fluid to flow from the first end to the second end.
- Optionally, the indirect flow conduit includes a spiral protrusion helically wrapped around the flow-through conduit and radially protruding from the flow-through conduit away from the center axis.
- Optionally, the spiral protrusion that radially protrudes from the flow-through conduit is configured to extend from the flow-through conduit to an inner surface of the larger exterior conduit.
- Optionally, the spiral protrusion is configured to be helically wrapped around the flow-through conduit at least partially between a first end and a second end of the flow-through conduit along the center axis.
- Optionally, the spiral protrusion is configured to create a flow path for the second portion of the fluid to flow helically along the spiral protrusion between a first end and a second end of the flow-through conduit.
- Optionally, the indirect flow conduit includes one or more closed loops radially protruding from the flow-through conduit on opposite sides of the center axis.
- Optionally, the one or more closed loops creates a longer flow path for the second portion of the fluid to flow from the first end to the second end relative to a flow path created by the flow-through conduit for the first portion of the fluid to flow from the first end to the second end.
- Optionally, the one or more closed loops that radially protrude from the flow-through conduit are configured to create a flow path for the second portion of the fluid to flow around the one or more closed loops between a first end and a second end of the flow-through conduit.
- In one embodiment of the subject matter described herein, an inline fluid damper device includes plural elongated stems that couple with each other at plural nodes. The stems form an elongated flow-through conduit extending around a center axis. The flow-through conduit is configured to be placed inside a larger exterior conduit through which a fluid flows. The stems are configured to dampen one or more of flow fluctuations or pressure fluctuations in the fluid flowing in the larger exterior conduit by dividing the fluid such that at least some of the fluid flows through the flow-through conduit without contacting the stems and at least some of the fluid concurrently flows through the flow-through conduit and contacts the stems.
- Optionally, the stems are configured to extend from the flow-through conduit to an inner surface of the larger exterior conduit.
- Optionally, the stems are configured to protrude from the plural nodes in a direction towards the center axis.
- Optionally, the plural stems are configured to form a lattice extending around the center axis between a first end and a second end of the flow-through conduit.
- In one embodiment of the subject matter described herein, an inline fluid damper device includes a flow-through conduit configured to be placed inside a larger exterior conduit through which a fluid flows. The flow-through conduit is elongated and extends around a center axis. The damper device also includes an indirect flow conduit coupled with the flow-through conduit. The indirect flow conduit is also configured to be placed inside the larger exterior conduit. The flow-through conduit and the indirect flow conduit are configured to dampen one or more flow fluctuations or pressure fluctuations in the fluid flowing in the larger exterior conduit by dividing the fluid into a first portion that flows along the center axis through the flow-through conduit and a second portion that concurrently flows outside of the flow-through conduit along the center axis and along a different direction. The flow-through conduit is configured to extend from a first end to a second end. The indirect flow conduit creates a longer flow path for the second portion of the fluid to flow from the first end to the second end relative to a flow path created by the flow-through conduit for the first portion of the fluid to flow from the first end to the second end.
- Optionally, the indirect flow conduit includes a spiral protrusion helically wrapped around the flow-through conduit and radially protruding from the flow-through conduit away from the center axis.
- Optionally, the spiral protrusion is configured to be helically wrapped around the flow-through conduit at least partially between a first end and a second end of the flow-through conduit along the center axis.
- Optionally, the spiral protrusion is configured to create a flow path for the second portion of the fluid to flow helically along the spiral protrusion between a first end and a second end of the flow-through conduit.
- Optionally, the spiral protrusion that radially protrudes from the flow-through conduit is configured to extend from the flow-through conduit to an inner surface of the larger exterior conduit.
- Optionally, the indirect flow conduit includes one or more closed loops radially protruding from the flow-through conduit on opposite sides of the center axis.
- Optionally, the one or more closed loops creates a longer flow path for the second portion of the fluid to flow from the first end to the second end relative to a flow path created by the flow-through conduit for the first portion of the fluid to flow from the first end to the second end.
- As used herein, an element or step recited in the singular and proceeded with the word “a” or “an” should be understood as not excluding plural of said elements or steps, unless such exclusion is explicitly stated. Furthermore, references to “one embodiment” of the presently described subject matter are not intended to be interpreted as excluding the existence of additional embodiments that also incorporate the recited features. Moreover, unless explicitly stated to the contrary, embodiments “comprising” or “having” an element or a plurality of elements having a particular property may include additional such elements not having that property.
- It is to be understood that the above description is intended to be illustrative, and not restrictive. For example, the above-described embodiments (and/or aspects thereof) may be used in combination with each other. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the subject matter set forth herein without departing from its scope. While the dimensions and types of materials described herein are intended to define the parameters of the disclosed subject matter, they are by no means limiting and are exemplary embodiments. Many other embodiments will be apparent to those of skill in the art upon reviewing the above description. The scope of the subject matter described herein should, therefore, be determined with reference to the appended claims, along with the full scope of equivalents to which such claims are entitled. In the appended claims, the terms “including” and “in which” are used as the plain-English equivalents of the respective terms “comprising” and “wherein.” Moreover, in the following claims, the terms “first,” “second,” and “third,” etc. are used merely as labels, and are not intended to impose numerical requirements on their objects. Further, the limitations of the following claims are not written in means-plus-function format and are not intended to be interpreted based on 35 U.S.C. § 112(f), unless and until such claim limitations expressly use the phrase “means for” followed by a statement of function void of further structure.
- This written description uses examples to disclose several embodiments of the subject matter set forth herein, including the best mode, and also to enable a person of ordinary skill in the art to practice the embodiments of disclosed subject matter, including making and using the devices or systems and performing the methods. The patentable scope of the subject matter described herein is defined by the claims, and may include other examples that occur to those of ordinary skill in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims.
Claims (20)
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US15/827,587 US10808874B2 (en) | 2017-11-30 | 2017-11-30 | Inline fluid damper device |
| CN201811443689.XA CN109854386B (en) | 2017-11-30 | 2018-11-29 | Inline fluid damper device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US15/827,587 US10808874B2 (en) | 2017-11-30 | 2017-11-30 | Inline fluid damper device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| US20190162350A1 true US20190162350A1 (en) | 2019-05-30 |
| US10808874B2 US10808874B2 (en) | 2020-10-20 |
Family
ID=66634361
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US15/827,587 Active 2038-02-21 US10808874B2 (en) | 2017-11-30 | 2017-11-30 | Inline fluid damper device |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US10808874B2 (en) |
| CN (1) | CN109854386B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3943734A1 (en) * | 2020-07-24 | 2022-01-26 | Pratt & Whitney Canada Corp. | Hydraulic snubber insert for gas turbine engine and associated method of installation |
| US12085022B2 (en) | 2019-10-07 | 2024-09-10 | Pratt & Whitney Canada Corp. | Aircraft fluid system pressure variation attenuation |
| EP4650661A1 (en) * | 2024-05-15 | 2025-11-19 | General Electric Company | Turbine engine having a multicavity damper |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12297699B2 (en) * | 2021-05-07 | 2025-05-13 | Mitchell Z. Dziekonski | Vibration damping subsea tubular system |
| US12134986B1 (en) | 2024-01-23 | 2024-11-05 | General Electric Company | Acoustic damping device |
Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1236987A (en) * | 1915-10-19 | 1917-08-14 | Nat Silencer Company | Muffler. |
| US1505893A (en) * | 1920-03-06 | 1924-08-19 | Hunter William | Silencer for internal-combustion engines |
| US1612584A (en) * | 1922-09-30 | 1926-12-28 | Hunter William | Silencer for internal-combustion engines |
| US1782396A (en) * | 1929-01-29 | 1930-11-25 | Fairchild Aviat Corp | Muffler |
| US2359365A (en) * | 1943-05-20 | 1944-10-03 | Katcher Morris | Muffler |
| US3700069A (en) * | 1971-05-20 | 1972-10-24 | Gen Motors Corp | Wave interference silencer |
| US3913703A (en) * | 1974-05-03 | 1975-10-21 | Gen Motors Corp | Single inner assembly wave interference silencer |
| US3963092A (en) * | 1975-03-05 | 1976-06-15 | Soares John M | Exhaust muffler for competition car engines |
| US4050539A (en) * | 1975-09-13 | 1977-09-27 | Teruo Kashiwara | Exhaust apparatus for internal combustion engine |
| US4683978A (en) * | 1984-11-22 | 1987-08-04 | Tula Silencers (Propriety) Limited | Exhaust silencer |
| US20050011700A1 (en) * | 2003-07-14 | 2005-01-20 | Dadd Paul M. | Devices for regulating pressure and flow pulses |
| US7117973B2 (en) * | 2001-12-22 | 2006-10-10 | Mann & Hummel Gmbh | Noise suppressor apparatus for a gas duct |
| US20160201530A1 (en) * | 2015-01-09 | 2016-07-14 | Flexible Metal Inc. | Split path silencer |
Family Cites Families (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1329559A (en) | 1916-02-21 | 1920-02-03 | Tesla Nikola | Valvular conduit |
| US3235003A (en) | 1963-06-04 | 1966-02-15 | Cloyd D Smith | Spiral flow baffle system |
| US5076782A (en) | 1989-07-26 | 1991-12-31 | Campbell Johnny E | Control device for a fuel valve |
| US5685157A (en) | 1995-05-26 | 1997-11-11 | General Electric Company | Acoustic damper for a gas turbine engine combustor |
| US6038862A (en) | 1997-12-23 | 2000-03-21 | United Technologies Corporation | Vibration damper for a fuel nozzle of a gas turbine engine |
| WO2001049975A1 (en) | 2000-01-06 | 2001-07-12 | Damping Technologies, Inc. | Turbine engine damper |
| US6948479B1 (en) | 2004-09-01 | 2005-09-27 | Delphi Technologies, Inc. | Inline pulsation damper system |
| WO2006029421A1 (en) * | 2004-09-17 | 2006-03-23 | Julius Blum Gmbh | Fluid damper |
| US7600607B2 (en) | 2005-11-17 | 2009-10-13 | John Timothy Sullivan | Flow-through sound-cancelling mufflers |
| US7966819B2 (en) | 2006-09-26 | 2011-06-28 | Parker-Hannifin Corporation | Vibration damper for fuel injector |
| CN101476738B (en) * | 2008-01-03 | 2011-04-06 | 西北农林科技大学 | Fluid damping device |
| KR101600296B1 (en) * | 2010-08-18 | 2016-03-07 | 한온시스템 주식회사 | Double pipe heat exchanger and manufacturing method the same |
| KR101671600B1 (en) | 2012-02-24 | 2016-11-16 | 미츠비시 쥬고교 가부시키가이샤 | Acoustic damper, combustor and gas turbine |
| US9074565B2 (en) | 2012-07-16 | 2015-07-07 | Denso International America, Inc. | Damped fuel delivery system |
| EP2865948B1 (en) | 2013-10-25 | 2018-04-11 | Ansaldo Energia Switzerland AG | Gas turbine combustor having a quarter wave damper |
| EP3034945B1 (en) | 2014-12-19 | 2018-05-30 | Ansaldo Energia Switzerland AG | Gas turbine fuel pipe comprising a damper |
-
2017
- 2017-11-30 US US15/827,587 patent/US10808874B2/en active Active
-
2018
- 2018-11-29 CN CN201811443689.XA patent/CN109854386B/en active Active
Patent Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1236987A (en) * | 1915-10-19 | 1917-08-14 | Nat Silencer Company | Muffler. |
| US1505893A (en) * | 1920-03-06 | 1924-08-19 | Hunter William | Silencer for internal-combustion engines |
| US1612584A (en) * | 1922-09-30 | 1926-12-28 | Hunter William | Silencer for internal-combustion engines |
| US1782396A (en) * | 1929-01-29 | 1930-11-25 | Fairchild Aviat Corp | Muffler |
| US2359365A (en) * | 1943-05-20 | 1944-10-03 | Katcher Morris | Muffler |
| US3700069A (en) * | 1971-05-20 | 1972-10-24 | Gen Motors Corp | Wave interference silencer |
| US3913703A (en) * | 1974-05-03 | 1975-10-21 | Gen Motors Corp | Single inner assembly wave interference silencer |
| US3963092A (en) * | 1975-03-05 | 1976-06-15 | Soares John M | Exhaust muffler for competition car engines |
| US4050539A (en) * | 1975-09-13 | 1977-09-27 | Teruo Kashiwara | Exhaust apparatus for internal combustion engine |
| US4683978A (en) * | 1984-11-22 | 1987-08-04 | Tula Silencers (Propriety) Limited | Exhaust silencer |
| US7117973B2 (en) * | 2001-12-22 | 2006-10-10 | Mann & Hummel Gmbh | Noise suppressor apparatus for a gas duct |
| US20050011700A1 (en) * | 2003-07-14 | 2005-01-20 | Dadd Paul M. | Devices for regulating pressure and flow pulses |
| US20160201530A1 (en) * | 2015-01-09 | 2016-07-14 | Flexible Metal Inc. | Split path silencer |
| US9500108B2 (en) * | 2015-01-09 | 2016-11-22 | Flexible Metal, Inc. | Split path silencer |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12085022B2 (en) | 2019-10-07 | 2024-09-10 | Pratt & Whitney Canada Corp. | Aircraft fluid system pressure variation attenuation |
| EP3943734A1 (en) * | 2020-07-24 | 2022-01-26 | Pratt & Whitney Canada Corp. | Hydraulic snubber insert for gas turbine engine and associated method of installation |
| US11608927B2 (en) | 2020-07-24 | 2023-03-21 | Pratt & Whitney Canada Corp | Hydraulic snubber insert for gas turbine engine and associated method of installation |
| EP4650661A1 (en) * | 2024-05-15 | 2025-11-19 | General Electric Company | Turbine engine having a multicavity damper |
Also Published As
| Publication number | Publication date |
|---|---|
| US10808874B2 (en) | 2020-10-20 |
| CN109854386A (en) | 2019-06-07 |
| CN109854386B (en) | 2022-01-28 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10808874B2 (en) | Inline fluid damper device | |
| EP2384401B1 (en) | Broadband silencer | |
| US4402485A (en) | Eccentrically nested tube gas line silencer | |
| CN101016853B (en) | Silencer | |
| US9618151B2 (en) | Compact modular low resistance broadband acoustic silencer | |
| EP3183441B1 (en) | Valvular-conduit manifold | |
| JP6392643B2 (en) | rectifier | |
| JP2018503022A (en) | Air pipes for intake pipes of internal combustion engines, especially automobiles | |
| CN109555871B (en) | Flow Stabilizers for Control Valves | |
| JPH06241854A (en) | Vortex flowmeter | |
| US20120273298A1 (en) | Silencers for air conditioning systems | |
| RU150274U1 (en) | ENGINE RELEASE SYSTEM (OPTIONS) | |
| JP2017015043A (en) | Exhaust heat recovery device | |
| RU150646U1 (en) | ENGINE RELEASE SYSTEM (OPTIONS) | |
| JP2008240586A (en) | Vehicular muffler | |
| US9399936B2 (en) | Exhaust apparatus | |
| US12006854B2 (en) | Vehicle exhaust system | |
| JP2008050989A (en) | Silencer | |
| US11639676B2 (en) | Vehicle exhaust system | |
| KR101692579B1 (en) | Muffler for Vehicle with Multi Path | |
| JP6381417B2 (en) | Silencer | |
| RU119062U1 (en) | DEVICE FOR EXTINGUISHING THE PRESSURE PULSATION | |
| JP2015021424A (en) | Muffler for vehicle | |
| JP3206344U (en) | Inner silencer | |
| WO2022196100A1 (en) | Air intake duct for internal combustion engine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: GENERAL ELECTRIC COMPANY, NEW YORK Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:SAMARASINGHE, RAMAL JANITH;MAGINA, NICHOLAS ARTHUR;WICKERSHAM, ANDREW;AND OTHERS;SIGNING DATES FROM 20171129 TO 20171130;REEL/FRAME:044264/0516 |
|
| FEPP | Fee payment procedure |
Free format text: ENTITY STATUS SET TO UNDISCOUNTED (ORIGINAL EVENT CODE: BIG.); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: NON FINAL ACTION MAILED |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: RESPONSE TO NON-FINAL OFFICE ACTION ENTERED AND FORWARDED TO EXAMINER |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: NON FINAL ACTION MAILED |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: RESPONSE TO NON-FINAL OFFICE ACTION ENTERED AND FORWARDED TO EXAMINER |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: FINAL REJECTION MAILED |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: RESPONSE AFTER FINAL ACTION FORWARDED TO EXAMINER |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: NON FINAL ACTION MAILED |
|
| STPP | Information on status: patent application and granting procedure in general |
Free format text: NOTICE OF ALLOWANCE MAILED -- APPLICATION RECEIVED IN OFFICE OF PUBLICATIONS |
|
| STCF | Information on status: patent grant |
Free format text: PATENTED CASE |
|
| MAFP | Maintenance fee payment |
Free format text: PAYMENT OF MAINTENANCE FEE, 4TH YEAR, LARGE ENTITY (ORIGINAL EVENT CODE: M1551); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY Year of fee payment: 4 |